[0001] This application is a continuation-in-part of co-pending application entitled "Non-Steady-State
Self-Regulating Intermittent Flow Thermodynamic System" filed March 25, 1993 and given
Serial No. 08/036,901, the applicant of which is one of the applicants of the present
application, and co-pending continuation-in-part application entitled "Circulation
of Oil in Refrigeration Systems with Immiscible Refrigerant-Oil Combinations" filed
June 20, 1994 and given Serial No. 08/262,680, the applicants of which are the same
as those of the present application.
Background of the Invention
[0002] This invention concerns an extension of the technology described in the aforementioned
related co-pending applications, particularly with respect to inclusion of pulsed
ejectors in combination with nozzling devices which generate high velocity bursts
of substantially unrestricted refrigerant flow throughout a refrigeration system.
United States Patent No. 5,240,384 describes a refrigeration system utilizing ejectors
having partitioned mixing tubes or diffusers to create multiple flow passages in each
of which the primary high velocity fluid jet stream effectively pulses. However that
pulsation is an internal process within the ejector body and it does not change the
conventional steady-state continuous fluid flow throughout the system. In contrast
the concept upon which the present invention is based is that of a substantially non-steady-state
intermittent flow throughout the entire system.
[0003] Refrigeration cycles typically include a vapor compressor, a condenser which changes
vapor to liquid as it gives off heat, an expansion device reducing the refrigerant
pressure, and an evaporator changing liquid to vapor as it provides cooling. Expansion
devices of the prior art are inefficient because of energy loss during the throttling
process. Also optimum use of evaporator surface area is limited when conventional
expansion devices are used because of the requirement of substantial superheat of
refrigerant vapor by a portion of the evaporator. For highest efficiency the entire
surface area of an evaporator should be fully wetted but with conventional expansion
devices full wetting of the evaporator surface is not possible because the compressor
must be protected from wet gas or liquid.
[0004] Evaporator and condenser heat exchange tubing of the prior art is typically of serpentine
configuration with horizontal tubing having a multiplicity of U-bends. An appreciable
pressure drop is inherent in such heat exchanger designs in order to move oil along
with the refrigerant and achieve appropriate heat transfer rates. High pressure drops
lower overall system efficiency and increase the compressor pumping power requirements.
Also, horizontal evaporator and condenser tubing can result in laminar non-turbulent
flow with associated low heat transfer rates. Condensed liquid tends to fill the lower
half of each horizontal run of tubing thereby reducing the available surface area
left for heat transfer. Lengthy runs of heat exchange tubing with a multiplicity of
U-bends cannot be arranged vertically because if they were oil flow would be impeded
and that could lead to compressor failure.
[0005] Defrosting of conventional evaporator heat exchanger tubes in ordinary refrigeration
systems is a lengthy energy-intensive process. It is one of the objects of the present
invention to render a refrigeration system reversible so that it can function alternatively
as a heat pump and dispose quickly and efficiently of accumulated evaporator frost.
[0006] Metering systems are known in the prior art for steady-state throttling of refrigerant
flow. Typically the mechanical throttling restriction is modulated in response to
either temperature or pressure changes in the system related to superheat of the refrigerant
vapor. In contrast the technology of self-regulation of a thermodynamic system described
in the earlier of the aforementioned related applications is extended by the present
invention to the sensing of both pressure and temperature to provide feedback to a
setpoint switch which continuously modulates the operating setpoint. As the setpoint
modulates, the magnitude of the sensed temperature and sensed pressure at each moment
of the system operation can vary with changing environmental conditions. One object
of the present invention is to rely upon no fixed temperature or pressure setpoint.
Momentary temperature and pressure operating setpoints are relational and their magnitude
varies as the system self-regulates with changing environment conditions.
Summary of the Invention
[0007] A refrigeration system is the subject of this invention wherein a refrigerant circulates
from an evaporator to a compressor to a condenser and thence back to the evaporator
through a nozzling device. That device includes a nozzle and a valve automatically
fully opened and closed in a binary fashion to create accelerated intermittent high
velocity bursts of substantially unrestricted refrigerant flow from an outlet of the
nozzle through the system. The system of the invention comprises a pulsed ejector
having a pulsed ejection suction port into which the refrigerant is directed form
the nozzle outlet. A pulsed ejector suction conduit connects the pulsed ejector suction
port with refrigerant flow between the evaporator and the compressor. The evaporator
includes a plurality of substantially vertical evaporator tubes interconnected in
parallel by lower and upper evaporator headers. The nozzling device and pulsed ejector
when the nozzling device is open carries the refrigerant upwardly through the evaporator
from the lower to the upper evaporator headers so that liquid refrigerant wets substantially
all inner surfaces of the evaporator tubes. The pulsed ejector suction conduit recirculates
refrigerant leaving the upper header of the evaporator back to the pulsed ejector
when the nozzling device is open.
[0008] Sensing means may be included for sensing pressure and temperature of the refrigerant
in the system to open fully or close the valve in response to a change in at least
one of the system pressure and temperature. The sensing means may comprise a thermostatic
bulb sensing refrigerant temperature in the system and a pressure tap sensing refrigerant
pressure in the system to infinitely vary a setpoint at which the nozzling device
valve opens and closes. As a consequence momentary temperature and pressure operating
setpoints are relational and the magnitude of the sensed temperature and sensed pressure
at each moment of system operation varies as the system self-regulates with changing
environment conditions.
[0009] It is preferred that the condenser comprise a plurality of substantially vertical
condenser tubes interconnected in parallel by lower and upper condenser headers. A
condenser ejector may be included having a condenser ejector suction port for directing
refrigerant vapor from the compressor downwardly through the condenser tubes from
the upper to the lower condenser headers. A condenser ejector suction conduit may
connect the condenser ejector suction port with refrigerant flow from the lower condenser
header. The condenser ejector suction conduit recirculates refrigerant leaving the
lower condenser header back to the condenser ejector when the nozzling device valve
is open.
Recirculated refrigerant intimately mixing with the hot gas entering the ejector from
the compressor accomplishes a desuperheating of the superheated hot gas at heat transfer
coefficients greater than that of the 'dry-wall' desuperheating of hot gas in the
condensers of the prior art.
[0010] The condenser ejector suction port may direct refrigerant vapor from the compressor
to the lower condenser header. The nozzling device and pulsed ejector when the nozzling
device valve is open carries the refrigerant upwardly through the condenser tubes
from the lower to the upper condenser header so that liquid refrigerant condenses
on inner surfaces of the condenser tubes and flows downwardly in counterflow relation
to refrigerant vapor carried upwardly through the condenser tubes.
[0011] In one embodiment of the invention the upper condenser header is of dead-end form.
Hot gas from the compressor can enter the lower header, which also functions as a
refrigerant reservoir. The liquid refrigerant condensing on inner surfaces of the
condenser tubes then flows downwardly in counterflow relation to vapor carried upwardly
through the condenser tubes to the upper dead-end condenser header. Hot gas bubbling
up through the condensed liquid in the lower header is effectively completely desuperheated
prior to entering the vertical condenser tubes, leaving the entire tube surface area
available for condensing heat transfer.
[0012] Means may be included for selectively operating the system alternatively as a heat
pump system. This may include reversing valve means for reversing the direction of
refrigerant flow from a refrigeration mode to a heat pump mode. The condenser in the
refrigeration mode then functions as an evaporator in the heat pump mode and the evaporator
in the refrigeration mode then functions as a condenser in the heat pump mode when
the reversal of direction of flow occurs. In the heat pump mode the system may rapidly
melt frost accumulated on the evaporator tubes during operation in the refrigeration
mode.
[0013] The reversing valve means may be provided at the discharge of the compressor and
the outlet of the pulsed ejector for reversing the direction of refrigerant flow from
the refrigeration mode to the heat pump mode while utilizing a single nozzling device
and pulsed ejector.
[0014] The nozzling device and pulsed ejector may be duplicated as first and second nozzling
devices and pulsed ejectors. The reversing valve means for reversing the direction
of refrigerant flow from the refrigeration mode to the heat pump mode may be without
check valves. The first nozzling device and pulsed ejector meters refrigerant flow
in one direction and the second nozzling device and pulsed ejector meters flow in
the opposite direction. The condenser in the refrigeration mode then functions as
an evaporator in the heat pump mode and the evaporator in the refrigeration mode then
functions as a condenser in the heat pump mode when the first nozzling device and
pulsed ejector cease operation and the second nozzling device and pulsed ejector meter
flow in the opposite direction.
[0015] There may be by-pass reservoir means included in the system for withdrawing refrigerant
from the system in response to a reduction in system superheat and returning refrigerant
to the system in response to an increase in system superheat. As system superheat
rises and falls refrigerant alternately enters and leaves the reservoir means and
alternately enters and leaves the system.
[0016] The system may be an absorption system with an absorbent fluid and a refrigerant
each circulating in its own flow circuit. The nozzling device and pulsed ejector are
then duplicated as an absorber nozzling device and an absorber pulsed ejector and
a refrigerant nozzling device and a refrigerant pulsed ejector. The refrigerant may
pass from the refrigerant evaporator to the refrigerant pulsed ejector before entering
the absorber, so that the refrigerant pulsed ejector is in series with respect to
the absorber. Alternatively, the refrigerant may circulate directly from the evaporator
to the absorber without passing through the refrigerant pulsed ejector so that the
refrigerant pulsed ejector is in parallel with respect to the absorber.
[0017] Also contemplated as part of the invention are certain sub-combinations with the
refrigeration system wherein the refrigerant circulates from evaporator to compressor
to condenser and thence back to the evaporator through a nozzle device including a
nozzle and a valve automatically fully opened and closed in a binary fashion to create
accelerated intermittent high velocity bursts of substantially unrestricted refrigerant
flow from an outlet of the nozzle through the system. One such sub-combination comprises
a thermostatic bulb sensing refrigerant temperature in the system and a pressure tap
sensing refrigerant pressure in the system to infinitely vary a setpoint at which
the nozzling device opens and closes. Another such sub-combination comprises the condenser
with its plurality of substantially vertical condenser tubes interconnected in parallel
by lower and upper condenser headers and the condenser ejector with a condenser ejector
suction port for directing refrigerant from the compressor upwardly through the condenser
tubes from the lower to the upper condenser headers. A condenser ejector suction conduit
may connect the condenser ejector suction port with refrigerant flow from the upper
condenser header. The condenser ejector suction conduit recirculates refrigerant leaving
the upper condenser header back to the condenser ejector when the nozzling device
valve is open. When the nozzling device valve is open carrying the refrigerant upwardly
through the condenser tubes from the lower to the upper condenser headers, refrigerant
liquid then condenses on inner surfaces of the condenser tubes and flows downwardly
in counterflow relation to refrigerant vapor carried upwardly through the condenser
tubes. In this latter sub-combination the upper condenser header may be a dead-end
header.
[0018] Also included in the invention is the pulse velocity induced enhancement of heat
transfer within the condenser and evaporator without associated increases in heat
exchanger pressure drop or flow losses. A pulse flow event initiates external ejector
recirculation flows for each ejector. Due to the design of the condenser and evaporator
heat exchangers, the pulse velocity of a pulse flow event initiates internal ejector-related
recirculation effects within the condenser and evaporator heat exchangers, further
enhancing heat transfer.
[0019] Also included in the invention is a novel phenomenon resulting from the pulse high
velocity, high impulse mass flow rate flow events. The high velocity pulse flows produce
a potentially non-equilibrium process characterized by velocity induced subcooling
of condenser liquid. The high velocity, high impulse mass flow rate flows can result
in the flashing of condenser liquid to vapor. The increased liquid subcooling that
results increases overall system efficiency and cooling capacity.
[0020] Also included in the invention is a thermodynamic process wherein a heat exchange
fluid is circulated and wherein a method is provided of continual thermodynamic efficiency
self-optimization in real time as energy is exchanged in the process with an external
environment. In this method the heat exchange fluid is directed through a valve and
nozzle. The pressure of the heat exchange fluid in the system is sensed and the temperature
of the heat exchange fluid is sensed. The sensed temperature is converted to an equivalent
sensed pressure. The valve is automatically fully opened or closed in a binary fashion
in response to a change in the relation between the first pressure and the sensed
temperature thus permitting substantially unrestricted bursts of fluid flow through
the valve and permitting acceleration of the intermittent bursts of fluid flow by
the nozzle. The opening and closing of the valve in this method functions in a mechanical
feedback loop utilizing internal pressure information and internal temperature information
to self-regulate the opening and closing of the valve and flow through the nozzle.
Brief Description of the Drawings
[0021]
FIG. 1 is a schematic system according to the invention showing a continuously self-regulating
setpoint switch for regulating a pulsed ejector at the evaporator inlet in parallel
arrangement with the compressor and with a simple condenser ejector for condenser
overfeed;
FIG. 2 is a schematic similar to FIG. 1 with the system split for alternative heat
pump operation;
FIG. 3 is a schematic similar to FIG. 2 but in a unitary rather than split configuration
utilizing double pulsed ejectors;
FIG. 4 is a schematic of alternative heat pump configuration utilizing a single pulsed
ejector;
FIG. 5 is a schematic of a system according to the invention including refrigerant
by-pass storage and a dead-ended vertical condenser;
FIG. 6 is a schematic of a system of the invention for_absorption refrigeration with
a series ejector circuit for the absorbent flow pulsed ejector; and
FIG. 7 is an absorption system similar to FIG. 6 with a parallel ejector circuit for
the absorbent flow pulsed ejector.
Description of Preferred Embodiment
[0022] The term "refrigeration system" as used herein is to be understood as including an
air-conditioning system and a heat pump system.
[0023] The term "thermodynamic system" as used herein is to be understood as including a
refrigeration, air-conditioning system, and a heat pump system.
[0024] The term "thermodynamic fluid" as used herein is to be understood to mean a general
fluid, including homogeneous, heterogeneous, mixture, non-homogeneous, non-heterogeneous,
fraction, component, and blend, as descriptors of the fluid.
[0025] The term "pulsed ejector" as used herein is to be understood to mean a nozzling device
composed with an ejector body. A nozzling device is fundamentally composed of a valve
and a nozzle that are substantially unrestricting to fluid flow when the valve element
is open, the nozzle serving to accelerate fluid flow to the maximum attainable velocity.
An ejector body is fundamentally composed of a section communicating with the nozzle
of the nozzling device, a suction section, and a discharge section.
[0026] The term "simple ejector" or "simple pulsed ejector" as used herein is to be understood
to mean an ejector composed of a nozzle, a suction section, and a discharge section.
Said ejector experiences pulse fluid flow due to the action of a nozzling device within
a system without having the valve of said nozzling device situated immediately upstream
of said ejector. In general, the nozzle of a nozzling device and the nozzle of said
ejector are distinct and seperate entities.
[0027] The concept of internal recirculation flows within a heat exchanger as a result of
a high velocity pulse flow entering the heat exchanger is a fundamental extension
of the dynamical fact that momentum transfer and hence imparted fluid flow will occur
whenever fluid streams of different velocities interact. Said momentum transfer and
imparted fluid flow phenomenon are the basis upon which ejectors function.
[0028] The term "parallel" as used herein with respect to the orientation of an ejector
within a system to the other system elements is to be understood as generally utilized
with respect to electrical systems and electrical current flow. The analagous ejector
flow being the flow from the ejector suction port to the ejector discharge port. For
example, a "parallel" ejector orientation with respect to a heat exchanger and a compressor
generally increases fluid flow through the heat exchanger. The ejector recirculation
flow will impart a greater flow through the heat exchanger than than the flow through
the compressor, with the heat exchanger flow provided by the action of both the compressor
and the ejector. Were the ejector to cease to function, the heat exchanger would still
experience the compressor flow. Both the primary fluid flow entering the ejector through
the nozzle and the ejector suction flow is experienced by the heat exchanger as flow
through the heat exchanger. The combined nozzle and suction flow leaving the ejector
as the ejector discharge flow is experienced by the heat exchanger as flow through
the heat exchanger.
[0029] The term "series" as used herein with respect to the orientation of an ejector within
a system to the other system elements is to be understood as generally utilized with
respect to electrical systems and electrical current flow. The analagous ejector flow
being the flow from the ejector suction port to the ejector discharge port. For example,
a "series" ejector orientation with respect to a heat exchanger and a compressor generally
limits the fluid flow through the heat exchanger to that provided by the ejector suction
flow. The ejector suction flow can impart less flow through the heat exchanger than
than the flow through the compressor. Were the ejector to cease to function, the heat
exchanger would not experience the compressor flow. The primary fluid flow entering
the ejector through the nozzle is not experienced by the heat exchanger as flow through
the heat exchanger. Only the suction flow component of the combined nozzle and suction
flow leaving the ejector as the ejector discharge flow is experienced by the heat
exchanger as flow through the heat exchanger. The "no ejector suction flow, no heat
exchanger flow" aspect of "series" ejector piping has severely limited the use of
ejectors in refrigeration systems where the ejector efficiency and performance
[0030] In the refrigeration system shown in FIG. 1 a nozzling device 10 is associated with
an ejector body 11 to form a pulsed ejector. The nozzling device 10 includes a valve
element 12, a valve-nozzle transition section 13, and a nozzle composed of converging
nozzle inlet section 14, nozzle throat 15, and a diverging nozzle outlet section 16.
For a complete description of such a nozzling device and its operation see the aforementioned
copending application entitled Non-Steady-State Self-Regulating Intermittent Flow
Thermodynamic System. The ejector body 11 is composed of an ejector suction port 17,
a converging momentum transfer section 18, an ejector throat and mixing section 19,
a diverging diffuser pressure recovery section 20, and an ejector outlet section 21.
Depending on design considerations, the size, shape, and inclusion of nozzle, ejector,
and associated sections may vary.
[0031] The valve element 12 opens fully with substantially no restriction to fluid flow
and closes fully with no intermediate positions. The nozzle sections 14, 15, and 16
accelerate fluid flow to the maximum attainable velocity with substantially no restriction
to fluid flow. The nozzling device 10 achieves substantially isentropic flow when
open. High velocity fluid flow from the nozzle outlet 16 transfers momentum to fluid
within the ejector suction port 17 at the ejector converging momentum transfer section
18. High velocity fluid and entrained fluid from the ejector suction port 17 flow
through the converging section 18 to the ejector throat and mixing section 19 and
out of the ejector diverging diffuser section 20. In the ejector throat and mixing
section 19 the primary fluid and the entrained fluid mix. In the ejector diverging
diffuser section 20 some of the velocity of the fluid flow is recovered as a pressure
rise. Flow through the ejector is partially isentropic for minimal fluid flow losses,
the combined flow leaving through ejector outlet section 21.
[0032] The nozzling device 10 is actuated by a solenoid coil 23 which fully opens the valve
element 12 when energized and fully closes the valve element when deenergized. A setpoint
self-regulating pressure switch 24 regulates the operation of the solenoid coil 23.
An electrical conduit 25 transfers power between the electric contacts of the setpoint
switch 24 and the solenoid coil 23. An electrical conduit 26 supplies power to the
solenoid coil 23 through the contacts of the switch 24 and the conduit 25. Power from
the conduit 26 fully opens the nozzling device 10 when the contacts of the switch
24 complete an electrical circuit between 26, 25, and 23. When that circuit is broken
by the opening of the contacts of the switch 24, the solenoid coil 23 is deenergized
and the nozzling device 10 returns to its normally closed condition.
[0033] A conduit 28 transfers pressure information from the valve-nozzle transition section
13 within the nozzling device 10 to the setpoint switch 24. The conduit 28 is placed
close to the outlet of the valve element 12 so that there is an immediate sensing
of flow leaving the valve element 12. A conduit 29 transfers temperature information
from a thermostatic bulb 30 to the setpoint switch 24. Temperature information from
within a conduit 32 is transferred to the conduit 29 by the thermostatic bulb 30.
The conjunction of the temperature and pressure information continuously modulates
the momentary pressure and temperature setpoint of the setpoint switch 24. A compressor
33 functions to lower the pressure in the suction side of the system, and heat transferred
from the ambient to an evaporator heat exchanger 34 functions to raise the temperature
within the suction side of the system. The setpoint switch 24 opens the nozzling device
10 when the pressure-temperature relation rises above the switch setpoint, permitting
fluid to flow from within an upstream conduit 34 through the valve element 12 to the
valve-nozzle transition section 13. As the burst of fluid enters the transition section
13 and the high velocity fluid flows through an outlet conduit 35 it produces a pressure
rise within the suction side of the system, changing the pressure-temperature relation
between the sensed pressure and the sensed temperature. When the pressure-temperature
relation is below the switch setpoint the contacts of the setpoint switch 24 open
and the solenoid coil 23 deenergizes closing the nozzling device 10 and stopping fluid
flow through the nozzling device 10. With the nozzling device 10 closed the compressor
33 lowers the suction side pressure as heat transfer from the ambient raises the suction
side temperature until the pressure-temperature relation is above the switch setpoint,
resulting in the reopening of the nozzling device 10. As the nozzling device 10 alternates
between fully open and fully closed conditions, fluid alternately flows and does not
flow within the thermodynamic system.
[0034] The high velocity burst of fluid flows into the evaporator heat exchanger 36 through
the conduit 35 and out through a conduit 37. The evaporator heat exchanger 36 includes
a lower header 38 and an upper header 39 interconnecting in parallel an array of closely
spaced vertical evaporator tubes 40.
[0035] When the nozzling device 10 is open, suction within the pulsed ejector suction port
17 pulls refrigerant from an ejector suction conduit 41 to the ejector suction port
17. When the nozzling device 10 is closed the compressor 33 pulls refrigerant in the
reversed direction out of the ejector suction port 17 through the conduit 41, back
through the conduit 32, a counter-flow heat exchanger 42, a suction conduit 43, to
the inlet of the compressor 33. Accompanying the reversal of flow direction within
the ejector suction conduit 41 as the pulsed ejector opens and closes, pulling suction
at the ejector suction port 17 and ceasing to pull suction, is a pseudo reversal of
flow within the evaporator heat exchanger 36. The high velocity pulses of refrigerant
proceed through the tubes 40 of the evaporator heat exchanger 36 with virtually no
pressure drop. This results in a marked improvement in evaporator efficiency as compared
to prior art evaporator heat exchangers which include long lengths of tubing with
many U-bends. The liquid phase of the refrigerant passing through the evaporator heat
exchanger 36 thoroughly wets the inside of the surface of the tubes 40 throughout
their length which increases heat transfer. When the high velocity liquid contacts
the inside of the tubes 40, and the refrigerant within the tubes 40, the bulk flow
can change from laminar to turbulent which provides an additional increase in heat
transfer. The vapor phase of the refrigerant passes centrally through the tubes 40.
[0036] The compressor 33 continuously acts to remove refrigerant from the outlet of the
evaporator 36 through the conduit 37 and the inlet of the evaporator 36 as reversed
flow through the ejector suction conduit 41. The flow of refrigerant within the ejector
suction conduit 41 and the evaporator 36 experiences partial reversals with respect
to the continuous direction of flow caused by the compressor as the pulsed ejector
opens and closes. When the evaporator 36 is fabricated as a completely parallel heat
exchanger with upper and lower headers, the high velocity flow through the conduit
35 entering the lower header of the evaporator 36 can cause an ejector-type suction
by momentum transfer to the fluid within the vertical tubes 40. Thus the tubes of
the evaporator 36 become multiple ejector stages, resulting in recirculating flow
within the heat exchanger itself during a pulsed high velocity flow event, and a reversal
of flow direction within the multiple ejector tubes when a pulse event ceases.
[0037] Refrigerant from the conduit 41 and the conduit 37 flows through the conduit 32 to
the counter-flow heat exchanger 42. Fluid flows out of the counter-flow heat exchanger
42 through the conduit 43 to the compressor 33. The counter-flow heat exchanger 42
serves to further lower the temperature of the refrigerant leaving a condenser heat
exchanger 44 and entering the nozzling device 10 by exchanging heat with the lower
temperature refrigerant leaving the evaporator heat exchanger 36. The counter-flow
heat exchanger 42 need not be used in all applications.
[0038] The condenser heat exchanger 44 includes a lower header 45 and an upper header 46
interconnected by a plurality of vertical closely spaced tubes 47 much like the configuration
of the evaporator heat exchanger 36.
[0039] The compressor 33 transfers mechanical energy to the fluid, increasing the pressure
and temperature of the fluid and discharging it through a conduit 48 to a nozzle inlet
49 of a condenser refrigerant overfeed simple pulsed ejector 50. When the nozzling
device 10 opens to allow high impulse mass flow through the pulsed ejector body 11
and through the overall system, fluid flowing from a condenser overfeed ejector nozzle
body 51 through a converging nozzle section 52 increases in velocity. The high velocity
flow from the converging nozzle section 52 transfers momentum to fluid within a condenser
overfeed ejector suction port 53. High velocity fluid flow from the nozzle outlet
52 transfers momentum to fluid within the ejector suction port 53 at an ejector converging
momentum transfer section 54. High velocity fluid and entrained fluid from the ejector
suction port 53 flow through the converging section 54 to an ejector throat and mixing
section 55 and out of an ejector diverging diffuser section 56. In the ejector throat
and mixing section 55 the primary fluid and the entrained fluid mix. In the ejector
diverging diffuser section 56 some of the velocity of the fluid flow is recovered
as a pressure rise. Fluid flows from the diverging section 56 through an ejector outlet
57 and a conduit 58 to the upper header 46 of the condenser heat exchanger 44. Depending
on operating conditions, the size and shape of the ejector and nozzle sections and
the relative position of the nozzle to the ejector sections can vary. Flow through
the ejector is partially isentropic in the spirit of design for minimal fluid flow
losses.
[0040] Fluid flows out of the lower header 45 of the condenser heat exchanger 44 through
a conduit 59 to a conduit 60 to a filter-drier 61 which functions to filter out contaminants
and remove moisture from the refrigerant. A simple ejector suction conduit 62 supplies
refrigerant overfeed to the condenser overfeed ejector suction port 53. Filtered refrigerant
flows out of the filter-drier 61 through a conduit 63 to the counter-flow heat exchanger
42. The fluid that enters the counter-flow heat exchanger 42 through the conduit 63
in counter-flow heat relationship with fluid flowing from the heat exchanger 36 to
the compressor 33 emerges through the conduit 64, flows through a sight glass 65 and
the conduit 34 and returns to the nozzling device 10 to complete a thermodynamic cycle.
The sight glass 65 indicates the quality of the refrigerant in the system, and is
not required in all applications.
[0041] As the thermodynamic system functions as a mechanical feedback loop, the self-regulating
setpoint switch 24 will self-regulate the pressure and temperature setpoints at the
valve-nozzle transition section 13 and the thermostatic bulb 30 to maintain the differential
pressure between the conduit 29 and the conduit 28. As the self-regulation is relational,
the magnitude of the sensed pressures can be from the vacuum range to the high pressure
range, representing the entire range of pressures and temperatures that the refrigerant
and the thermodynamic system are able to maintain.
[0042] The condenser 44 in FIG. 1 may be fed with refrigerant in its lower header 45 as
will be described in reference to FIG. 2.
[0043] In the reversible heat pump system shown in FIG. 2, the fundamental components of
the FIG. 1 embodiment are arranged in a split heat pump system. Component parts 10
to 21, 23 to 26, 28 to 30, 32, 36, and 41 of FIG. 1, composing a pulsed ejector, a
setpoint self-regulating superheat switch, a heat exchanger, and interconnecting conduit
are repeated twice as A and B sub-systems in FIG. 2 as component parts having the
same reference numerals with A and B suffixes. Each of these functions in an analogous
fashion to the corresponding component parts of FIG. 1.
[0044] Similarly, component parts 49 to 57 of FIG. 1, composing a simple ejector, are repeated
twice in the A and B systems of FIG. 2 as component parts having the same reference
numerals with A and B suffixes. Each of these parts in the A and B sub-systems in
FIG. 2 functions in an analogous fashion to the corresponding component parts of FIG.
1.
[0045] Similarly, compressor 33, filter-drier 61, and sight glass 65 of FIG. 1 are repeated
in FIG. 2 as compressor 33A, filter-drier 61A and sight glasses 65A and 65B respectively
and they function in an analogous fashion to the corresponding component parts of
FIG.1. The critical elements that make FIG. 1 into a reversible heat pump in FIG.
2 are: a reversing valve 70, and check valves 71, 71A, 72 and 72A which enable the
direction of fluid flow through the system to reverse, switching the heat exchangers
from being condenser and evaporator respectively to being evaporator and condenser
respectively. In one operating mode, for example, the 'cooling' mode, the nozzling
device 10B remains closed while the nozzling device 10A pulses. In the other operating
mode, for example, the 'heating' mode, the nozzling device 10A remains closed while
the nozzling device 10B pulses. The respective heating and cooling mode refrigerant
flows are switched by the reversing valve 70.
[0046] One distinct difference in the circuit in FIG. 2 with respect to the circuit in FIG.
1 is the placement of the condenser overfeed ejector 50 of FIG. 1 relative to the
upper and lower header of the condenser 44 of FIG. 1. In FIG. 1, the condenser overfeed
ejector 50 is placed with its discharge section 57 at the upper header 46, and with
its suction port 53 in communication with the lower header 45 through the ejector
suction conduit 62. In FIG. 2, the condenser overfeed ejector 50A and the condenser
overfeed ejector 50B are placed with their respective ejector discharge sections 57A
and 57B in communication with the lower header 38A and 38B of the heat exchanger 36A
and 36B respectively; and with the suction ports 53A and 53B in communication with
the upper header 39A and 39B of the heat exchanger 36A and 36B respectively through
ejector suction conduits 62A and 62B respectively. In FIG. 1, the condenser 44 is
a 'top feed,' or 'upper header feed' condenser, with refrigerant entering the upper
header 46 first.
[0047] In FIG. 2, the purpose of the check valve 71 and the check valve 71A is to route
refrigerant so that the heat exchanger 36A and the heat exchanger 36B become 'bottom
feed,' or 'lower header feed' condensers, with refrigerant entering the lower header
38A or 38B first.
[0048] In any particular version of the circuits represented in FIG. 1 and FIG. 2, the position
and orientation of the condenser overfeed ejector can be in either the 'top feed'
or 'bottom feed' placements. For overall simplicity, the condenser overfeed ejector
can be removed completely from the system schematics, which would enable the removal
of the check valves 71 and 71A, and unnecessary associated conduits in FIG. 2 as well.
The spirit of FIG. 1 and FIG. 2 is to show representative piping schematics including
a condenser overfeed ejector that can be further simplified as required by circumstance
In either figure, the condensers can be piped as 'top feed or 'bottom feed' as required,
with or without condenser overfeed ejectors.
[0049] In the 'cooling mode,' the nozzling device 10B remains closed. As the nozzling device
10A alternates between fully open and fully closed conditions, fluid alternately flows
and does not flow within the thermodynamic system. With each pulse, a high velocity
burst of fluid flows from the conduit 35A through a condui 73 into the evaporator
heat exchanger 36A. When nozzling device 10A is open, suction within the pulsed ejector
suction port 17A pulls refrigerant from the upper header 39A of the evaporator 36A
through the ejector suction conduit 41A to the ejector suction port 17A. When the
nozzling device 10A is closed the compressor 33A pulls refrigerant in the reversed
direction out of ejector suction port 17A through the conduit 41A back to the inlet
of the compressor 33A. Similar flow reversal and secondar ejector effects within the
heat exchanger 36A occur as described with respect to heat exchanger 36 in FIG. 1.
[0050] Refrigerant flows out of the evaporator 36A from the conduit 58A and the conduit
59A. Refrigerant flowing through the conduit 58A flows backwards through the ejector
50A, flowing to the conduit 62A and a conduit 74. Refrigerant flow from the conduit
59A and the conduit 62A combines to flow through the conduit 37A. Refrigerant from
the conduit 37A flows through the check valve 71 to a conduit 76. Refrigerant from
the conduit 74 and the conduit 76 flows through the conduit 32A to the reversing valve
70. Refrigerant flows from the reversing valve 70 through the conduit 43A to the compressor
33A. The compressor 33A transfers mechanical energy to the fluid, increasing the pressure
and temperature of the fluid and discharging it through the conduit 48A to the reversing
valve 70. High pressure, high temperature refrigerant leaving the reversing valve
70 through the conduit 32B to a conduit 76A is prevented from entering the upper header
39B of the condenser 36B by the check valve 71A, resulting in the flow of refrigerant
through a conduit 74A to the condenser overfeed ejector 50B.
[0051] When the nozzling device 10A opens to allow high impulse mass flow through the pulsed
ejector body 11A and through the overall system, the condenser overfeed ejector 50B
functions in a manner similar to the condenser overfeed ejector 50 of Fig. 1. Entrained
fluid from the ejector suction port 53B flows from the ejector suction conduit 62B
which flows from the conduit 59B which flows from the upper header 39B of the condenser
36B.
[0052] When the condenser 36B is fabricated as a completely parallel heat exchanger with
upper and lower headers, and substantially vertical tubes, fluid flowing from the
conduit 58B enters the lower header 38B of the condenser 36B. The condensation process
becomes one of hot gas rising within the vertical tubes 40B, with condensed liquid
forming and falling down the tubes, establishing an internal counterflow of rising
gas and falling liquid. Condensed liquid is able to drain from the tube surface area
into the lower header 38B, which acts as a liquid receiver, leaving the inner tube
surface area available for condensing heat transfer. The entry of hot gas into a partially
liquid filled lower header enables a very rapid de-superheating of the hot gas due
to intimate contact with the liquid refrigerant, leaving the internal surface area
of the condenser available for condensing heat transfer and subcooling heat transfer,
which occurs at higher heat transfer coefficients than de-superheating heat transfer.
Thus the internal surface area becomes more effective than in heat exchangers that
devote a portion of their active internal tube surface area to the 'dry wall' de-superheating
heat transfer process. Condensed liquid and vapor overfeed flow out of the condenser
36B upper header 39B through the conduit 59B and through the ejector suction conduit
62B serves to further enhance heat transfer within the condenser 36B. The conduit
62B supplies refrigerant overfeed to the condenser overfeed ejector suction port 53B.
[0053] High velocity flow leaving the condenser overfeed ejector 50B through the conduit
58B entering the lower header 38B of the condenser 36B can cause an ejector-type suction
by momentum transfer to the fluid within the vertical tubes 40B. Thus the tubes of
the condenser 36B become multiple ejector stages, resulting in recirculating flow
within the heat exchanger itself during a pulsed high velocity flow event, and a reversal
of flow direction within the multiple ejector tubes when a pulse event ceases. The
flow reversals and counter-flow characteristics within the condenser tubes can be
considered natural convection processes when a pulse ceases, and forced convection
processes when a pulse flow occurs.
[0054] Fluid flows out of the condenser heat exchanger 36B through a conduit 73A, and is
prevented from flowing through the conduit 35B and the ejector body llB by pulsed
ejector valve element 12B, which remains closed. Condensed refrigerant from conduit
73A flows through a conduit 77A, through the check valve 72A, through a conduit 78A,
through a conduit 34B, through the sight glass 65B, through the conduit 64B, to the
filter-drier 61A which functions to filter out contaminants and remove moisture from
the refrigerant.
Filtered refrigerant flows through the conduit 64A, through the sight glass 65A to
the conduit 34A. Refrigerant is prevented from flowing through a conduit 78 by the
check valve 72. Refrigerant from the conduit 34A flows through a conduit 79, returning
to the nozzling device 10A to complete a thermodynamic cycle. The sight glass 65A
and the sight glass 65B are not required in all applications.
[0055] As the thermodynamic system functions as a mechanical feedback loop, the self-regulating
setpoint switch 24A will self-regulate the pressure and temperature setpoints at the
valve-nozzle transition section 13A and the thermostatic bulb 30A to maintain the
differential pressure between the conduit 29A and the conduit 28A which can be related
to a thermodynamic superheat.
[0056] To switch between 'cooling mode' and 'heating mode', reversing valve 70 is actuated.
Due to the substantial lack of flow restriction within the valve elements of both
pulsed ejectors, upon reversing modes the heat exchanger pressures equalize extremely
rapidly. This enables a rapid changeover between operating modes. In reversible heat
pumps of the prior art utilizing substantial flow restricting metering devices, a
significant delay is often required between switching heat pump modes to allow for
heat exchanger pressure equalization.
[0057] In the 'heating mode,' the nozzling device 10A remains closed. As nozzling device
10B alternates between fully open and fully closed conditions, fluid alternately flows
and does not flow within the thermodynamic system. With each pulse, a high velocity
burst of fluid flows from the conduit 35B through the conduit 73A into the lower header
38B of the evaporator heat exchanger 36B. When the nozzling device 10B is open, suction
within the pulsed ejector suction port 17B pulls refrigerant from the upper header
39B of the evaporator 36B through the ejector suction conduit 41B to the ejector suction
port 17B. When the nozzling device 10B is closed the compressor 33A pulls refrigerant
in the reversed direction out of the ejector suction port 17B through the conduit
41B back to the inlet of the compressor 33A. Similar flow reversal and secondary ejector
effects within the heat exchanger 36B occur as described with respect to the heat
exchanger 36 in FIG. 1.
[0058] Refrigerant flows out of the'evaporator 36B from the conduit 58B and the conduit
59B. Refrigerant flowing through the conduit 58B flows backwards through the ejector
50B, flowing to the conduit 62B and the conduit 74A. Refrigerant flow from conduit
59B and the conduit 62B combines to flow through the conduit 37B. Refrigerant from
conduit 37B flows through the check valve 71A to the conduit 76A. Refrigerant from
the conduit 74A and the conduit 76A flows through the conduit 32B to the reversing
valve 70. Refrigerant flows from the reversing valve 70 through the conduit 43A to
the compressor 33A.
[0059] The compressor 33A transfers mechanical energy to the fluid, increasing the pressure
and temperature of the fluid and discharging it through conduit 46A to the reversing
valve 70. High pressure, high temperature refrigerant leaving the reversing valve
70 through the conduit 32A to the conduit 76 is prevented from entering the upper
header 39A of the condenser 36A by the check valve 71, resulting in the flow of refrigerant
through the conduit 74 to the nozzle inlet 49A of the condenser overfeed ejector 50A.
[0060] When the nozzling device 10B opens to allow high impulse mass flow through the pulsed
ejector body 11B and through the overall system, fluid flows through the ejector 50A
and its associated conduits in a manner similar to that described for the ejector
50B and its associated conduits in the 'cooling mode' mentioned previously.
[0061] When the condenser 36A is fabricated as a completely parallel heat exchanger with
upper and lower headers, and substantially vertical tubes, fluid flowing from the
conduit 58A enters the lower header of the condenser 36A. The condensation process
becomes that described by the condenser 36B in the 'cooling mode' heretofore described.
[0062] Condensed liquid and vapor overfeed flow out of the condenser 36A upper header 39A
through the conduit 59A and through the ejector suction conduit 62A serves to further
enhance heat transfer within the condenser 36A. The conduit 62A supplies refrigerant
overfeed to the condenser overfeed ejector suction port 53A.
[0063] High velocity flow leaving the condenser overfeed ejector 50A through the conduit
58A entering the lower header 38A of the condenser 36A can cause an ejector-type suction
by momentum transfer to the fluid within the vertical tubes 40A as previously described.
[0064] Fluid flows out of the condenser heat exchanger 36A through the conduit 73, and is
prevented from flowing through the conduit 35A and the ejector body 11A by the pulsed
ejector valve element 12A, which remains closed. Condensed refrigerant from the conduit
73 flows through a conduit 77, through the check valve 72, through the conduit 78,
through the conduit 34A, through the sight glass 65A, through the conduit 64A, to
the filter-drier 61A. Filtered refrigerant flows through the conduit 64B, through
the sight glass 65B to the conduit 34B. Refrigerant is prevented from flowing through
the conduit 78A by the check valve 72A. Refrigerant from the conduit 34B flows through
a conduit 79A, returning to the nozzling device 10B to complete a thermodynamic cycle.
[0065] As the thermodynamic system functions as a mechanical feedback loop, the self-regulating
setpoint switch 24B will self-regulate the pressure and temperature setpoints at the
valve-nozzle transition section 13B and the thermostatic bulb 30B to maintain the
differential pressure between the conduit 29B and the conduit 28B which can be related
to a thermodynamic superheat.
[0066] In the reversible heat pump system shown in FIG. 3, the fundamental components of
FIG. 2 are arranged in a unitary heat pump system with a bi-directional pulsed ejector
10C made possible by bi-directional flow through a valve element 12C, which is actuated
by a solenoid coil 23C.
[0067] Component parts in FIG. 3 with the same reference numerals as in FIG. 1 and FIG.
2 function in an analogous fashion as in those other embodiments. Suffixes C and D
are used here in FIG. 3 for parts corresponding to the numerals with A and B suffixes
in FIG. 2.
[0068] The critical element that makes the FIG. 3 embodiment into a reversible unitary heat
pump is a bi-directional flow through valve element 12C. This enables a reversing
valve 70A to change the diredtion of fluid flow through the system without the need
for check valves. In one operating mode, for example, the 'cooling' mode, a bi-directional
pulsed ejector 10C meters refrigerant flow in one direction, from the condenser heat
exchanger 36D into the evaporator heat exchanger 36C, actuated by the self-regulating
setpoint switch 24C. In the other operating mode, for example, the 'heating' mode,
the bi-directional pulsed ejector 10C meters refrigerant flow in the opposite direction,
from the condenser heat exchanger 36C into the evaporator heat exchanger 36D, actuated
by the self-regulating setpoint switch 24D. The respective heating and cooling mode
refrigerant flows are switched by the reversing valve 70A.
[0069] In FIG. 3, the purpose of the check valve 71B and the check valve 71C is to route
refrigerant so that the heat exchanger 36C and the heat exchanger 36D become 'bottom
feed', or 'lower header feed' condensers, with refrigerant entering the lower header
first.
[0070] In FIG. 3, a condenser overfeed ejector could be installed in either the 'top feed'
or 'bottom feed' placements as described in FIG. 1 and FIG. 2. For overall simplicity,
the condensers could be piped as 'top feed', which would enable the removal of the
check valves 71B and 71C, and the connecting conduits 74C, 37C, 76B, and 74D, 37D,
76C as well. The spirit of FIG. 1, FIG. 2, and FIG. 3 is to show representative piping
schematics, including condenser overfeed ejectors, that can be further simplified
or augmented as required by circumstance. In each figure, the condensers can be piped
as 'top feed' or 'bottom feed' as required.
[0071] In the 'cooling mode,' as the bi-directional pulsed ejector 10C alternates between
fully open and fully closed conditions, fluid alternately flows and does not flow
within the thermodynamic system. With each pulse, a high velocity burst of fluid flows
from the conduit 35C into the lower header 38C of the evaporator heat exchanger 36C.
When the valve element 12C is open, suction within the pulsed ejector suction port
17C pulls refrigerant from the upper header 39C of the evaporator 36C through the
ejector suction conduit 41C to the ejector suction port 17C. When the valve element
12C is closed the compressor 33B pulls refrigerant in the reversed direction out of
the ejector suction port 17C through the conduit 41C back to the inlet of the compressor
33B. Similar flow reversal and secondary ejector effects within the heat exchanger
36C occur as described with respect to the heat exchanger 36A in FIG. 2.
[0072] Refrigerant flows out of the evaporator 36C from the conduit 74C and the conduit
37C. Refrigerant from the conduit 37C flows through the check valve 71B to the conduit
76B. Refrigerant flow from the conduit 76B and the conduit 74C combines to flow through
the conduit 32C. Refrigerant from the conduit 32C flows to the reversing valve 70A.
Refrigerant flows from the reversing valve 70A through the conduit 43B to the compressor
33B.
[0073] The compressor 33B transfers mechanical energy to the fluid, increasing the pressure
and temperature of the fluid and discharging it through the conduit 48B to the reversing
valve 70A. High pressure, high temperature refrigerant leaving the reversing valve
70A through the conduit 32D to the conduit 76C is prevented from entering the upper
header 39D of the condenser 36D by the check valve 71C, resulting in the flow of refrigerant
through the conduit 74D to the lower header of the condenser 36D. When the condenser
36D is fabricated as a completely parallel heat exchanger with upper and lower headers,
the condensing process is similar to that described for the condenser 36B of FIG.
2.
[0074] Fluid flows out of the condenser heat exchanger 36D through the conduit 35D. Refrigerant
from the conduit 35D flows backwards through the ejector body 11D which consists of
sections 21D, 20D, 19D, 18D and 17D, and backwards through the ejector nozzle which
consists of 16D, 15D and 14D, until the flow reaches the valve-nozzle transition section
13D. When the valve element 12C opens, fluid from the valve-nozzle transition section
13D flows through valve element 12C to the valve-nozzle transition section 13C. The
pulse of fluid flows through the nozzle and the ejector body into the evaporator 36C
as previously described.
[0075] To switch between 'cooling mode' and 'heating mode,' the reversing valve 70A is actuated.
When the heat exchanger 36C functions as an evaporator, the self-regulating setpoint
switch 24C actuates the bi-directional pulsed ejector 10C. When the heat exchanger
36D functions as an evaporator, self-regulating setpoint switch 24D actuates the bi-directional
pulsed ejector 10C.
[0076] To accomplish the rapid hot gas defrost, a rapid defrost switch 80 transfers electrical
power from the conduit 26E to the conduit 25E which transfers power to actuate reversing
valve 70A to reverse the direction of refrigerant flow. This reversal of flow sends
hot gas to what was previously the evaporator, to accomplish the defrosting of the
heat exchanger. When the defrosting is substantially completed the rapid defrost switch
80 actuates the reversing valve 70A to return to the prior flow direction, allowing
the defrosted heat exchanger to resume function as an evaporator.
flows and does not flow within the thermodynamic system. With each pulse, a high velocity
burst of fluid flows from the conduit 35D into the evaporator heat exchanger 36D.
when the valve element 12C is open, suction within the pulsed ejector suction port
17D pulls refrigerant from the upper header 39D of the evaporator 36D through the
ejector suction conduit 41D to the ejector suction port 17D. When the valve element
12C is closed the compressor 33B pulls refrigerant in the reversed direction out of
the ejector suction port 17D through the conduit 41D back to the inlet of the compressor
33B. Similar flow reversal and secondary ejector effects within the heat exchanger
36D occur as described with respect to the heat exchanger 36A in FIG. 2.
[0077] Refrigerant flows out of the evaporator 36D from the conduit 74D and the conduit
37D. Refrigerant from the conduit 37D flows through the check valve 71C to the conduit
76C. Refrigerant flow from the conduit 76C and the conduit 74D combines to flow through
the conduit 32D. Refrigerant from the conduit 32D flows to the reversing valve 70A.
Refrigerant flows from the reversing valve 70A through the conduit 43B to the compressor
33B.
[0078] The compressor 33B transfers mechanical energy to the fluid, increasing the pressure
and temperature of the fluid and discharging it through the conduit 48B to the reversing
valve 70A. High pressure, high temperature refrigerant leaving the reversing valve
70A through the conduit 32C to the conduit 76B is prevented from entering the upper
header 39C of the condenser 36C by the check valve 71B, resulting in the flow of refrigerant
through the conduit 74C to the lower header 38C of the condenser 36C. When the condenser
36C is fabricated as a completely parallel heat exchanger with upper and lower headers,
the condensing process is similar to that described for the condenser 36B of FIG.
2.
[0079] Fluid flows out of the condenser heat exchanger 36C through the conduit 35C. Refrigerant
from the conduit 35C flows backwards through the ejector body 11C which consists of
the sections 21C, 20C, 19C, 18C and 17C and backwards through the ejector nozzle which
consists of the sections 16C, 15C and 14C until the flow reaches the valve-nozzle
transition section 13C. When the valve element 12C opens, fluid from the valve-nozzle
transition section 13C flows through the valve element 12C to the valve-nozzle transition
section 13D. The pulse of fluid flows through the nozzle and the ejector body into
the evaporator 36D as previously described.
[0080] As the thermodynamic system functions as a mechanical feedback loop, when the heat
exchanger 36C functions as an evaporator, the self-regulating setpoint switch 24C
will self-regulate the pressure and temperature setpoints at the valve-nozzle transition
section 13C and the thermostatic bulb 30C to maintain the differential pressure between
the conduit 29C and the conduit 28C which can be related to a thermodynamic superheat.
[0081] As the thermodynamic system functions as a mechanical feedback loop, when the heat
exchanger 36D functions as an evaporator, the self-regulating setpoint switch 24D
will self-regulate the pressure and temperature setpoints at the valve-nozzle transition
section 13D and the thermostatic bulb 30D to maintain the differential pressure between
the conduit 29D and the conduit 28D which can be related to a thermodynamic superheat.
[0082] In the reversible heat pump system shown in FIG. 4, the fundamental components of
FIG. 2 are arranged in a unitary heat pump system with a single pulsed ejector 10D
and two reversing valves, 70B and 70C. The reversing valve 70B switches the compressor
33C hot gas discharge flow to the heat exchanger 36E or to the heat exchanger 36F
depending on the mode of operation. The reversing valve 70C switches pulsed ejector
discharge flow to the heat exchanger 36F or to the heat exchanger 36E depending on
the mode of operation. Thus a single pulsed ejector can be utilized in a reversible
heat pump circuit. Any liquid refrigerant returning to a suction accumulator 82 is
recirculated through the heat exchanger acting as an evaporator due to suction flow
from the pulsed ejector 10D. The valve element 12D of the pulsed ejector 10D is actuated
by the solenoid coil 23D.
[0083] Component parts 24E, 25F, 26F, 28E, 29E, 30E and 11E of FIG. 4, function in an analogous
fashion to the corresponding component parts 24B, 25B, 26B, 28B, 29B, 30B and 11B,
respectively, of FIG. 2.
[0084] Other component parts in FIG. 4 with the same reference numerals as in FIG. 1 function
in an analogous fashion as in FIG. 1.
[0085] In one operating mode, for example, the 'cooling' mode, the pulsed ejector 10D meters
refrigerant flow through the conduit 37E to the reversing valve 70C. Refrigerant from
the reversing valve 70C flows through the conduit 73E into the evaporator heat exchanger
36E. Refrigerant leaving the evaporator 36E through the conduit 32F enters the reversing
valve 70B. Refrigerant entering the reversing valve 70B from the conduit 32F leaves
the reversing valve 70B through the conduit 83. The thermostatic bulb 30E senses the
temperature of the refrigerant within the conduit 83. Refrigerant from the conduit
83 flows into the suction accumulator 82.
phase leaves suction accumulator 82 through the conduit 43C to enter the compressor
33C. Compressed refrigerant leaves compressor 33C through the conduit 48C to enter
the reversing valve 70B. Refrigerant entering the reversing valve 70B from the conduit
48C leaves the reversing valve 70B through the conduit 32E. Refrigerant from the conduit
32E enters the condenser heat exchanger 36F. Refrigerant leaves the condenser 36F
through the conduit 73F to enter the reversing valve 70C. Refrigerant entering the
reversing valve 70C from the conduit 73F leaves the reversing valve 70C through the
conduit 34C to enter pulsed ejector 10D.
[0086] Liquid or vapor refrigerant from the suction accumulator 82 leaves through the conduit
41E due to the suction action of the pulsed ejector suction port 17E. An optional
check valve may be placed within the conduit 41E to prevent refrigerant liquid from
reversing direction and flowing from the ejector suction port 17E through the conduit
41E back into the accumulator 82.
[0087] The conjunction of bulb temperature 30E and system pressure at 13E determines the
actuation of the pulsed ejector 10D for metering refrigerant into the evaporator 36E
from the condenser 36F.
[0088] In the other operating mode, for example, the 'heating' mode, the pulsed ejector
10D meters refrigerant flow through the conduit 35E to the reversing valve 70C. Refrigerant
from the reversing valve 70C flows through the conduit 73F into the evaporator heat
exchanger 36F. Refrigerant leaving the evaporator 36F through the conduit 32E enters
the reversing valve 70B. Refrigerant entering the reversing valve 70B from the conduit
32E leaves the reversing valve 70B through the conduit 83. The thermostatic bulb 30E
senses the temperature of the refrigerant within the conduit 83. Refrigerant from
the conduit 83 flows into the suction accumulator 82. Refrigerant in the vapor phase
leaves suction accumulator 82 through the conduit 43C to enter the compressor 33C.
Compressed refrigerant leaves the compressor 33C through the conduit 48C to enter
the reversing valve 70B. Refrigerant entering the reversing valve 70B from the conduit
48C leaves the reversing valve 70B through the conduit 32F. Refrigerant from the conduit
32F enters the condenser heat exchanger 36E. Refrigerant leaves the condenser 36E
through the conduit 73E to enter the reversing valve 70C. Refrigerant entering the
reversing valve 70C from the conduit 73E leaves the reversing valve 70C through the
conduit 34C to enter the pulsed ejector 10D.
[0089] The conjunction of bulb temperature 30E and system pressure at 13E determines the
actuation of the pulsed ejector 10D for metering refrigerant into the evaporator 36F
from the condenser 36E.
[0090] Recirculation of liquid refrigerant from suction accumulator 82 through an evaporator
heat exchanger enables the liquid refrigerant to evaporate and provide cooling capacity
for the system.
[0091] When necessary, rapid defrosting may be accomplished by switching from heating mode
to cooling mode for the duration of the defrost cycle, and then switching back to
heating mode. Condenser overfeed ejectors and associated piping can be added as required.
[0092] The part load refrigerant storage system shown in FIG. 5 is a result of the ability
of pulsed metering devices to effectively meter refrigerant of any quality; subcooled
liquid, saturated liquid, two phase, and vapor. The purpose of the part load refrigerant
management system is to vary the cooling capacity of a system by varying the quality
of the refrigerant leaving the condenser by varying the active refrigerant charge
within the system. The cooling capacity in the evaporator is relative to the condenser
leaving liquid quality, with the most cooling capacity for subcooled liquid, less
for saturated liquid, less for two phase, and less for vapor.
[0093] In a typical system, one charges the system until there is subcooled liquid present
leaving the condenser. This is accomplished by adding refrigerant charge until a liquid
line sight glass is full, and the liquid temperature is below the saturation temperature
of the liquid pressure, indicating thermodynamic subcooling. A superheat measurement
is made at the evaporator outlet for the desired saturation evaporator temperature,
in order to determine whether there is sufficient cooling capacity. In order to lower
superheat and increase cooling capacity, more refrigerant charge is added to the system
to increase the condenser subcooling. In order to raise the superheat and decrease
cooling capacity, refrigerant is removed from the system to decrease the condenser
subcooling.
[0094] In the expansion systems of the prior art, a "liquid seal" at the expansion device
inlet is typically required, which requires some degree of liquid subcooling as a
result. Thus the removal of refrigerant charge to decrease cooling capacity at low
load is not practical, lest saturated or two phase refrigerant enter the expansion
device causing faulty system operation. As a result, refrigeration systems of the
prior art have difficulty operating at low load conditions effectively, often utilizing
inefficient means of false loading the compressor such as hot gas bypass, where hot
gas is bypassed from the compressor outlet directly back to the compressor inlet,
forcing the compressor to do pumping work without doing any cooling with the bypassed
flow. The other method of lowering load is to reduce the evaporator pressure, and
thus temperature. This can lead to dropping the evaporator temperature below 32 F,
resulting in frosting over, and blockage of the evaporator, which can lead to compressor
failure due to excessive liquid floodback. In compressors that have performance curves
that are very sensitive to suction pressure and density, such as centrifugal compressors,
going to lower load conditions by lowering evaporator pressure can result in very
poor efficiency and performance at low loads.
[0095] The present invention functions by bypassing condenser outlet refrigerant into a
reservoir when evaporator outlet superheat drops, which lowers the condenser pressure
and liquid subcooling by removing refrigerant charge from the active system loop.
As necessary due to low load and low superheat, refrigerant can be bypassed into the
reservoir until the condensing leaving refrigerant is two phase, and even just vapor,
resulting in lower cooling capacity in the evaporator. As superheat rises, refrigerant
from the reservoir is returned to the active refrigerant system loop by entering the
evaporator, increasing the active refrigerant charge, which increases the condenser
pressure and lowers the quality of the refrigerant leaving the condenser. Just as
in charging the system initially, the condenser leaving refrigerant will go from vapor
to two phase to saturated to subcooled, as refrigerant is added to the active system
loop. The lower the quality of the condenser leaving refrigerant, the higher the cooling
capacity in the evaporator. Thus the refrigerant bypass storage system manages low
and high load conditions by varying the quality of the refrigerant leaving the condenser.
As the pulsed ejector can effectively meter any quality refrigerant, performance of
the overall system remains within required operating realms.
[0096] In the embodiment of the refrigerant bypass storage system shown in FIG. 5, the pulsed
ejector 10E is actuated by the pressure switch 24F. Electric power from the conduit
26G enters the pressure switch 24F, and is transferred through the conduit 25G to
the solenoid coil 23E when the switch contacts within the pressure switch 24F are
closed, completing an electric circuit between the conduit 26G, the pressure switch
24F, the conduit 25G, and the solenoid coil 23E. When the switch contacts within the
pressure switch 24F are opened, breaking the electric circuit between the conduit
26G, the pressure switch 24F, the conduit 25G, and the solenoid coil 23E electric
power ceases to flow. Pressure switch 24F actuates the solenoid coil 23E, which opens
and closes the valve element 12E, metering refrigerant flow to maintain a pressure
setpoint. The pressure switch 24F receives pressure information from the system through
the conduit 28F, which senses pressure at the valve-nozzle transition section 13F.
The pressure switch 24F opens the valve element 12E on a drop in sensed pressure below
the pressure setpoint, and closes the valve element 12E on a rise in sensed pressure
above the pressure setpoint. The opening and closing of the substantially unrestricted
valve element 12E causes high velocity pulsed flow events through the valve body that
are sensed by the pressure switch 24F, resulting in a mechanical feedback loop self-regulation
of pulse rate and flow to maintain the pressure setpoint.
[0097] The pressure setpoint of the pressure switch 24F can be, for example, the pressure
at which the compressor 33D achieves optimum performance. As load variations change,
the pressure switch 24F will maintain the evaporator pressure at the optimum point,
and the refrigerant bypass system will vary the condenser leaving refrigerant quality
based on evaporator outlet superheat, effectively modulating evaporator cooling capacity.
Regulating system performance by refrigerant bypass based on a superheat determination
is useful in that the compressor requires a certain minimum superheat to avoid damage,
and the effective use of the evaporator surface area depends on a minimum, regulated
superheat. For example, given that a means of providing superheat to the evaporator
outlet refrigerant is provided within the system, the evaporator could be run with
a fully wetted surface area, increasing evaporator performance and cooling capacity,
increasing system performance with the compressor still protected from damage by refrigerant
liquid or wet vapor. Load management with the refrigerant bypass modulation of condenser
leaving refrigerant quality maintains the system performance and efficiency within
operating requirements as operating conditions vary.
[0098] In the refrigeration system, the practical requirement of the refrigerant bypass
system and bypass reservoir is to have sufficient refrigerant to return to the active
system at high loads, and sufficient volume to store refrigerant at low loads. Most
importantly, the relative levels of refrigerant in the active system and in the reservoir
should be self-regulated to maintain optimum system performance and efficiency as
operating conditions vary. This self-regulated balance can occur due to the conjunction
of a pressure switch for regulating evaporator pressure and a superheat switch for
regulating refrigerant bypass into the reservoir. Other combinations of system variables,
such as pressure, temperature, superheat, subcooling, and concentration, can be utilized
to self-regulate system operation and refrigerant bypass storage and release.
[0099] In the part load refrigeration storage system shown in FIG. 5, the thermostatic bulb
30F transfers temperature information from the evaporator 36G outlet conduit 32G to
the superheat switch 24G through the conduit 29F. System pressure information is transferred
to the superheat switch 24G through the conduit 28G and the conduit 85, which senses
pressure at the valve-nozzle transition element 13F. The superheat switch 24G can
be composed of a differential pressure switch acting on the difference in pressure
between the conduit 28G representing system pressure and the conduit 29F representing
pressure within the thermostatic bulb 30F. The superheat switch 24G acts to allow
refrigerant to enter a bypass reservoir 86 on a drop in the sensed differential pressure,
which can be related to a drop in superheat, and acts to allow refrigerant to leave
the bypass reservoir 86 on a rise in the sensed differential pressure, which can be
related to a rise in superheat.
[0100] On a rise in sensed superheat, electrical power from the conduit 26H is transferred
by the superheat switch 24G through the conduit 25I to the solenoid coil 23G, which
opens the solenoid valve 10G, allowing refrigerant from the bypass reservoir 86 to
leave through a conduit 87, flow through solenoid valve 10G, flow through a conduit
85 and enter the active system loop through the valve-nozzle transition element 13F.
The solenoid valve 10F is closed.
[0101] On a drop in sensed superheat, electrical power from the conduit 26H is transferred
by the superheat switch 24G through the conduit 25H to the solenoid coil 23F, which
opens the solenoid valve 10F, allowing condensed refrigerant from the conduit 90 to
flow through the solenoid valve 10F, through the conduit 91 and enter the bypass reservoir
86. The solenoid valve 10G is closed.
[0102] As superheat rises and falls, refrigerant alternately enters and leaves the reservoir
86, alternately entering and leaving the active system circuit.
[0103] As the pressure switch 24F maintains evaporator pressure, the superheat switch 24G
maintains evaporator superheat. The conjunction of the pressure switch 24F and the
superheat switch 24G act to handle load variations.
[0104] In FIG. 5, components 33D, 48D, 61B, 64C, 65C, 34D and 79B function in an analogous
fashion to the corresponding component parts 33A, 48A, 61A, 64B, 65B, 34B and 79A
respectively, of FIG. 2. The condenser heat exchanger 36H includes a lower header
38E, parallel vertical tubes 40C and a dead-ended upper header 39E. It is a 'bottom
feed' condenser fed with hot gas from the conduit 48D, with condensed liquid leaving
from the bottom header through the conduit 59A. Hot superheated gas from the compressor
discharge enters the lower header 38E from one end, rises into the tubes 40C, condenses,
setting up an internal turbulent counterflow of hot gas rising within the tubes 40C
and condensed liquid falling down the tube walls to collect in the lower header 38E.
As liquid fills the lower header 38E the hot gas very rapidly de-superheats by the
intimate mixing process of bubbling through the condensed liquid. Condensed, and even
subcooled liquid refrigerant leaves the lower header 38E through the conduit 59A at
the end opposite to the hot gas inlet from the conduit 48D with each high velocity
pulse event.
[0105] The pulsed ejector 10E, ejector body 11E, and their component parts function in analogous
fashion to the pulsed ejector 10A, ejector body 11A, and their component parts of
FIG. 2. The only substantial difference is that the pulsed ejector 10E is actuated
by the pressure switch 24F, whereas the pulsed ejector 10A is actuated by the superheat
switch 24A. The heat pump system in FIG. 2 will vary load by self-regulating superheat,
and by raising and lowering evaporator pressure and temperature as required. The refrigeration
system in FIG. 5 will vary load by self-regulating at a relatively fixed evaporator
pressure and temperature.
[0106] In FIG. 6, the pulsed ejector 10H regulates the flow of a refrigerant to an evaporator
heat exchanger 36I in which the refrigerant takes on heat from the environment to
be cooled. The refrigerant vapor then flows into an absorber 93 where it is absorbed
by thermodynamic fluid in the liquid state, releasing heat energy in an exothermic
process to the ambient environment. A pump 94 pressurizes the liquid from the absorber
93, pumping it through a counter-flow heat exchanger 95 into a vapor generator 96.
The high pressure liquid in the vapor generator 96 absorbs heat energy from a higher
temperature ambient source, releasing the refrigerant vapor absorbed into the liquid
in the absorber 93 as a high pressure and high temperature vapor. The high pressure
and high temperature refrigerant vapor flows from the vapor generator 96 to a rectifier
97 which removes any water in the liquid or vapor phase from the refrigerant vapor.
In some applications the rectifier 97 is not required; for example, when water is
the refrigerant. The dry vapor leaving the rectifier 97 condenses into liquid refrigerant
in the condenser heat exchanger 44A which releases heat energy to the ambient environment.
Liquid refrigerant from the condenser 44H flows to the inlet of the pulsed ejector
10H to complete a thermodynamic cycle.
[0107] Liquid absorbent fluid from the vapor generator 96 flows back through a conduit 98
to the counter-flow heat exchanger 95, where it exchanges heat energy with fluid flowing
from the pump 94 to the vapor generator 95, and then through a conduit 99 to the pulsed
ejector 10I which opens and closes to meter absorbent fluid flow back to the absorber
93.
temperature information, alternately opening and closing the pulsed ejector 10H. The
pulsed ejector 10H replaces a throttling expansion valve in systems of the prior art.
[0108] Absorbent fluid continually cycles through its system loop in an intermittent fashion
as the differential pressure switch 24J responds to internal pressure information,
alternately opening and closing the pulsed ejector 10I. The pulsed ejector 10I replaces
a throttling metering valve in systems of the prior art.
[0109] Both the pulsed ejector 10H and the pulsed ejector 10I recover energy wasted in the
throttling devices of the systems of the prior art. In systems where there are additional
throttling devices, the throttling devices can be replaced with pulsed ejectors, or
simple ejectors that do not include actuated valve elements.
[0110] The pulsed ejector absorption refrigeration system in FIG. 6 includes a condenser
overfeed ejector 50C, the pulsed ejector 10H feeding the evaporator 36I and providing
for recirculation, and the pulsed ejector 10I feeding the absorber 93 and providing
flow assist in moving fluid from the evaporator 36I to the absorber 93.
[0111] The solenoid-actuated pulsed ejector 10H is actuated by the solenoid coil 23J which
fully opens the valve element 12H when electrically energized and fully closes the
valve element 12H when deenergized. The superheat switch 24I regulates the energization
and de-energization of the solenoid coil 23J. The electrical conduit 25K transfers
electrical power between the electric contacts of the superheat switch 24I and the
solenoid coil 23J. The electrical conduit 26J supplies electrical power to the solenoid
coil 23J through the electric contacts of the switch 24I and the electrical conduit
25K.
[0112] Electric power from the conduit 26J fully opens the pulsed ejector 10H when the contacts
of the switch 24I complete an electrical circuit between 26J, 25K, and 23J. When the
electrical circuit between them is broken by the opening of the electrical contacts
of the switch 24I, the solenoid coil 23J is deenergized and the pulsed ejector 10H
returns to its normally closed condition.
[0113] The conduit 28H transfers pressure information from within the valve-ejector transition
section 13I to the superheat switch 24I. The conduit 29I transfers pressure information
from within the thermostatic bulb element 30I to the superheat switch 24I. The thermostatic
bulb 30I senses system temperature at the evaporator outlet conduit 32I. The differential
pressure at which the superheat switch 24I is set to open the pulsed ejector 10H is
chosen by design criterion. Thermodynamic criterion other than superheat can be utilized
to the actuate pulsed ejector 10H.
[0114] As the pump 94 lowers the pressure in the suction side of the thermodynamic system,
and heat energy is added to the evaporator 36I, the superheat switch 24I opens the
pulsed ejector 10H when the differential pressure between the bulb 30I pressure and
the system pressure at the valve-ejector transition section 13I, which can be related
to a superheat equivalent, rises above the differential pressure setting of the superheat
switch 24I, permitting flow of the thermodynamic fluid from within the upstream system
conduit 34E through the pulsed ejector 10H to the downstream system conduit 35I.
[0115] As the high velocity burst of thermodynamic fluid enters the valve-ejector transition
section 13I and flows to the downstream conduit 35I it produces an internal system
pressure rise within the suction side of the system. Refrigerant flowing through the
evaporator 36I to the outlet conduit 32I can lower the temperature as sensed by the
thermostatic bulb 30I, lowering its internal bulb pressure.
[0116] When the differential pressure sensed by the superheat switch 24I drops below the
differential pressure setpoint of the superheat switch 24I, the electric contacts
of the superheat switch 24I open and the solenoid coil 23J deenergizes closing the
valve element 12H within the pulsed ejector 10H, and stopping thermodynamic fluid
flow through the pulsed ejector 10H.
[0117] With the pulsed ejector 10H closed, the pump 94 lowers the suction side pressure,
and heat addition to the evaporator 36I can raise the temperature sensed at the evaporator
outlet conduit 32I by the thermostatic bulb 30I, the differential pressure sensed
by the superheat switch 24I rises above its differential pressure setpoint, resulting
in the reopening of the pulsed ejector 10H.
[0118] As the pulsed ejector 10H alternates between fully open and fully closed conditions,
refrigerant fluid alternately flows and does not flow within the thermodynamic system.
[0119] The pulsed ejector 10H component parts of FIG. 6 function in an analogous fashion
to the corresponding pulsed ejector 10 component parts of FIG. 1.
[0120] In FIG. 6, the ejector suction conduit 41G is shown recirculating fluid from what
can be construed to be the upper header 39F of a parallel, vertical, evaporator 36I.
[0121] The high velocity burst of thermodynamic fluid flows into the lower header 38I of
the evaporator heat exchanger 36I through the conduit 35I, resulting in internal recirculation
flows within evaporator 36I as previously described. Fluid flows out of evaporator
36I through the ejector suction conduit 32I to the ejector suction port 17J of the
pulsed ejector 10I. When the pulsed ejector 10I is closed, refrigerant fluid from
the conduit 32I may still flow through the body of the pulsed ejector 10I, flowing
through the ejector suction port 17J, the converging section 18J, the ejector throat/bore
section 19J, the diverging diffuser section 20J, the ejector outlet section 21J, flowing
through the conduit 35J to enter the absorber 93.
[0122] Refrigerant from the evaporator 36I is absorbed by the liquid absorbent fluid within
the absorber 93 in what is typically an exothermic process, releasing heat energy
to the external environment. Liquid absorbent fluid is pumped out of the absorber
93 through a conduit 100 by pump 94.
[0123] The pump 94 raises the pressure of the liquid absorbent fluid and discharges the
pressurized liquid through a conduit 101 to the counter-flow heat exchanger 95. Pressurized
liquid absorbent fluid that enters the counter-flow heat exchanger 95 through the
conduit 101 leaves through a conduit 102 and enters the vapor generator 96. Heat energy
from a higher temperature ambient environment is transferred to the vapor generator
96 so that refrigerant vapor is released from the absorbent fluid in an endothermic
process.
[0124] The high pressure refrigerant vapor leaves the vapor generator 96 through a conduit
103 and flows to the rectifier 97 which functions as a desiccant to remove any water
in the liquid or vapor phase from the refrigerant vapor. Dry refrigerant vapor leaves
the rectifier 97 through a conduit 104 and enters a simple condenser overfeed ejector
50C prior to entering the condenser heat exchanger 44A.
[0125] In FIG. 6, simple pulsed ejector 50C and its component parts function in an analogous
fashion to simple pulsed ejector 50 and component parts in FIG. 1. Discharge flow
from simple pulsed ejector 50C flows through conduit 58C to the upper header 39G of
condenser heat exchanger 44A.
[0126] The ejector suction conduit 62C is shown recirculating fluid from what can be construed
to be the lower header 45A of a parallel, vertical, condenser 44A.
[0127] Dry refrigerant vapor within the condenser heat exchanger 44A changes thermodynamic
state to refrigerant liquid as it releases heat energy to heat the external environment.
Liquid refrigerant leaves the condenser 44A through the conduit 34E and flows to the
inlet of the pulsed ejector 10H to complete a thermodynamic cycle.
[0128] High pressure liquid absorbent fluid from the vapor generator 96 leaves through the
conduit 98 and flows through the counter-flow heat exchanger 95, where it transfers
heat energy to absorbent fluid flowing from the pump 94 to the vapor generator 96,
preheating the absorbent fluid before it enters the vapor generator 96. Liquid absorbent
fluid entering the counter-flow heat exchanger 95 through the conduit 98 leaves the
counter-flow heat exchanger 95 through the conduit 99 and flows to the inlet of the
pulsed ejector 10I.
[0129] The pulsed ejector 10I opens and closes to meter absorbent fluid flow back to the
absorber 93, with the pulsed suction flow assisting the pump in moving fluid from
the evaporator 36I to the absorber 93.
[0130] The solenoid-actuated pulsed ejector 10I is actuated by the solenoid coil 23K which
fully opens the valve element 12I when electrically energized and fully closes the
valve element 12I when deenergized. The differential pressure switch 24J regulates
the energization and de-energization of the solenoid coil 23K. The electrical conduit
25L transfers electrical power between the electric contacts of the differential switch
24J and the solenoid coil 23K. The electrical conduit 26K supplies electrical power
to the solenoid coil 23K through the electric contacts of the switch 24J and the electrical
conduit 25L.
[0131] Electric power from the conduit 26K fully opens the pulsed ejector 10I when the contacts
of the switch 24J complete an electrical circuit. When the electrical circuit is broken
by the opening of the electrical contacts the solenoid coil 23K is deenergized and
the pulsed ejector 10I returns to its normally closed condition.
[0132] The basic premise of the self-regulated pulsed actuation of the absorbent flow pulsed
ejector 10I is as follows:
[0133] With the pulsed ejector 10H and pulsed ejector 10I normally closed, the pump 94 acts
to lower the pressure within the suction side of the system, seeking to maintain an
evaporator pressure and temperature as self-regulated by the superheat switch 24I
as it meters refrigerant flow. The pulsed ejector 10I has the active criterion of
metering absorbent fluid flow back to the absorber, at the absorber pressure that
is fundamentally determined by the superheat switch 24I. With the expectation of a
minimal amount of pressure drop from the evaporator to the absorber, pulsed ejector
10I has the active criterion of metering absorbent fluid back to the absorber at a
pressure slightly lower than the evaporator pressure.
[0134] Take, for example, a pressure difference of 1 PSIA, pounds per square inch absolute,
between the evaporator and the absorber; with the evaporator 1 PSIA higher than the
absorber. To maintain this, one places the differential pressure switch 24J in communication
with the evaporator pressure, in communication with the absorber pressure, and in
communication with the absorber pulsed ejector 10I.
[0135] The conduit 28I transfers pressure information from within the valve-ejector transition
section 13J, sensing absorber inlet pressure, to the differential pressure switch
24J. The conduit 29J transfers pressure information from within the valve-ejector
transition section 13I, sensing evaporator inlet pressure, to the differential pressure
switch 24J.
[0136] The differential pressure at which the differential pressure switch 24J is set to
open the pulsed ejector 10I is chosen by design criterion. Thermodynamic criterion
other than differential pressure may be utilized to actuate the pulsed ejector 10I.
For example, a differential pressure switch seeking to maintain discharge side pressures,
such as condenser outlet pressure and absorbent pressure at the inlet of absorbent
pulsed ejector 10I.
[0137] As the pump 94 lowers the pressure in the suction side of the thermodynamic system,
and heat energy is added to the evaporator 36I, the superheat switch 24I opens the
pulsed ejector 10H when the differential pressure between the bulb 30I pressure and
the system pressure at the valve-ejector transition section 13I, which can be related
to a superheat, rises above the differential pressure setting of the superheat switch
24I, permitting flow of the thermodynamic fluid from the refrigerant discharge side
of the thermodynamic system through the pulsed ejector 10H to the refrigerant suction
side of the thermodynamic system; producing an internal system pressure rise within
the suction side of the system.
[0138] The rise in pressure within the suction side of the system is first noted at the
valve-ejector transition section 13I as it is the closest location to the mass influx
through the pulsed ejector valve element 12H. The rise in suction pressure is thus
sensed simultaneously by the superheat switch 24I through the conduit 28H and sensed
by the differential pressure switch 24J through the conduit 29J.
[0139] When the differential pressure between the valve-ejector transition section 13I and
the valve-ejector transition section 13J sensed by the differential pressure switch
24J rises above the differential pressure setpoint of the differential pressure switch
24J, the electric contacts of the differential pressure switch 24J close and the solenoid
coil 23K energizes opening the valve element 12I within the pulsed ejector 10I, allowing
thermodynamic fluid flow through the pulsed ejector 10I.
[0140] Absorbent fluid flowing through pulsed ejector 10I into the absorber 93 raises the
absorber pressure, as sensed by the differential pressure switch 24J through the conduit
28I at the valve-ejector transition conduit 13J.
[0141] When the differential pressure between the valve-ejector transition section 13I and
the valve-ejector transition section 13J sensed by the differential pressure switch
24J drops below the differential pressure setpoint of differential pressure switch
24J, the electric contacts of the differential pressure switch 24J open and the solenoid
coil 23K deenergizes, closing the valve element 12I within the pulsed ejector 10I,
and stopping absorbent fluid flow through the pulsed ejector 10I.
[0142] As before, refrigerant flowing through the evaporator 36I to the outlet conduit 32I
can lower the temperature as sensed by the thermostatic bulb 30I, lowering its internal
bulb pressure.
[0143] When the differential pressure sensed by the superheat switch 24I drops below the
differential pressure setpoint of the superheat switch 24I, the electric contacts
of the superheat switch 24I open and the solenoid coil 23J deenergizes closing the
valve element 12H within the pulsed ejector 10H, and stopping refrigerant fluid flow
through the pulsed ejector 10H.
[0144] With the pulsed ejector 10H closed the pump 94 lowers the suction side pressure,
and heat addition to the evaporator 36I can raise the temperature sensed at the evaporator
outlet conduit 32I by the thermostatic bulb 30I, the differential pressure sensed
by the superheat switch 24I rises above its differential pressure setpoint, resulting
in the reopening of the pulsed ejector 10H.
[0145] With the pulsed ejector 10I closed the pump 94 lowers the suction side pressure within
the absorber to maintain the natural flow from evaporator to absorber, resulting in
a drop in the differential pressure sensed by the differential pressure switch 24J
below its differential pressure setpoint, resulting in the reopening of the pulsed
ejector 10I.
[0146] As the pulsed ejector 10H alternates between fully open and fully closed conditions,
refrigerant fluid alternately flows and does not flow within the thermodynamic system.
[0147] As the pulsed ejector 10I alternates between fully open and fully closed conditions,
absorbent fluid alternately flows and does not flow within the thermodynamic system.
[0148] The high velocity pulse mass flow flowing through absorbent fluid pulsed ejector
valve element 12I flows through the valve-ejector transition section 13J, through
the ejector body 11J which entails flow through the ejector nozzle 14J, the ejector
converging section 18J, the ejector throat/bore section 19J, the ejector diverging
diffuser section 20J, the ejector outlet section 21J through the conduit 35J into
the absorber 93.
[0149] High velocity pulse flow through the ejector nozzle 14J transfers momentum to fluid
within the ejector suction port 17J, which draws refrigerant from the evaporator 36I
through the ejector suction conduit 32I. The high velocity absorbent fluid flow and
the entrained refrigerant flow from the suction port 17J combine to flow through the
ejector sections 18J, 19J and 20J which function to recover some of the combined flow
velocity as a pressure rise. The pressure rise achieved lowers the pumping pressure
rise requirement of the pump 94 as the pulsed ejector 10I helps the pump move refrigerant
flow from the evaporator to the absorber.
[0150] The combined flow leaves the ejector body 11J through the ejector outlet section
21J, flowing through the conduit 35J to the absorber 93. The absorption process within
the absorber 93 is generally exothermic as refrigerant vapor is absorbed by absorbent
fluid. The high velocity pulsed flows and the inherent mixing within the ejector body
11J can be a means of improving absorber performance.
[0151] Absorbent fluid leaves the absorber 93 through the conduit 100 in a state of relatively
higher absorbed refrigerant concentration than the fluid entering pulsed ejector 10I.
The higher concentration absorbent fluid is returned to the pump 94 by the conduit
100 to continue the thermodynamic cycle.
[0152] The pulsed ejector absorption refrigeration system shown in FIG. 7 differs from that
shown in FIG. 6 in the relative orientations of the ejectors relative to the heat
exchangers and the absorber. The pulsed ejector absorption refrigeration system in
FIG. 7 includes a condenser overfeed ejector 50E, a pulsed ejector 10J feeding the
evaporator 34L and providing for recirculation of refrigerant, and a pulsed ejector
10K feeding the absorber 88A and providing for recirculation of absorbent fluid.
[0153] The evaporator outlet conduit 32J in FIG. 7 is analogous to the evaporator outlet
conduit 32I in FIG. 6 except that the evaporator outlet conduit 32J transfers refrigerant
directly to the absorber 88A, as opposed to the case in FIG. 6 where the evaporator
outlet conduit 32I transfers refrigerant directly to the pulsed ejector 10I prior
to entering the absorber 88.
[0154] In FIG. 7 the pulsed ejector suction conduit 41L, serves to recirculate absorbent
fluid leaving the absorber 93A through the conduit 100A. In contrast in FIG. 6 the
pulsed ejector suction conduit 32I, serves to assist the pump 94 in providing refrigerant
flow from the evaporator 36I to the absorber 93.
[0155] The spirit of the difference between the embodiments of FIG. 6 and FIG. 7 with respect
to the absorber pulsed ejector is the following:
[0156] The pulsed ejector 10I in FIG. 6 is in a series orientation with respect to the absorber
93 and the pump 94 so that the pulsed ejector provides a partial pressure rise to
the refrigerant prior to entering the absorber. The pulsed ejector 10K in FIG. 7 is
in a parallel orientation with respect to the absorber 93A and the pump 94A so that
the pulsed ejector provides an increased flow rate within the absorber 93A by recirculating
absorbent fluid through the absorber 93A.
[0157] The pulsed ejector 10K in FIG. 7 may have its ejector suction conduit 41L attached
at any point within the absorber 93A, accomplishing recirculation of absorbent fluid.
In FIG. 7 the component parts with the same numerical prefix as the component parts
in FIG. 6 function in an analagous fashion, respectively. The aforementioned component
parts of FIG. 6 and FIG. 7 differ in their alphanumeric suffixes, respectively.
[0158] In FIG. 7 the ejector suction conduit 41K is shown recirculating fluid from what
can be construed to be the lower header 38J of a parallel, vertical, evaporator 36J.
The ejector suction conduit 62D is shown recirculating fluid from what can be construed
to be the upper header 39I of a parallel, vertical, condenser 44B.
[0159] The simple pulsed condenser overfeed ejector 50D communicates fluid flow through
conduit 58D to the lower header 45B of the parallel, vertical condenser 44B, causing
internal recirculation flow as previously described.
[0160] The pulsed ejector 10J communicates fluid flow through conduit 35K to the upper header
39H of the parallel, vertical evaporator 36J, causing internal recirculation flow
as previously described.
[0161] Anticipating pulsed flow reversal phenomenon within the ejector suction recirculation
conduit 41L in FIG. 7, a check valve may be placed within that conduit to prevent
reversed flow from the ejector suction port 17L back to the pump 94A through the conduit
100B.
[0162] In the spirit of the invention, the relative communication of the ejectors to the
heat exchangers in can be in any combination of 'top feed', 'bottom feed', 'parallel',
and 'series'. In the event that the heat exchangers utilized in a particular embodiment
do not have headers, the relative communication of the ejectors to the heat exchangers
can be in any combination of 'parallel' and 'series' with respect to the means provided
to increase the pressure of and provide flow to the thermodynamic fluid within the
thermodynamic system.
[0163] The non-steady-state intermittent flow through the nozzling devices in the present
invention is a substantially isentropic nozzling process. The flow process through
the throttling valves in steady-state systems of the prior art is a substantially
isenthalpic throttling process. In a throttling device there is a distinct means of
flow restriction that results in fluid flow losses and a generation of entropy while
providing a pressure drop to steady-state flow. The flow restriction results in a
negligible velocity increase as fluid experiences a drop in pressure and temperature
in what is modeled thermodynamically as a constant enthalpy Joule-Thomson throttling
expansion process. The Joule-Thomson expansion process is the classical basis of steady-state
refrigeration, heat pump and air-conditioning cycles.
[0164] The nozzling devices are either fully open or fully closed with no intermediate positions,
with minimal flow restriction in the fully open condition. The absence of flow restriction
results in a substantially isentropic nozzling flow process and a substantial fluid
velocity increase as fluid experiences non-steady-state flow and a pressure drop.
The pressure difference between the inlet and the outlet of a nozzling device occurs
when fully closed. Inlet and outlet system pressures tend towards equalization when
the nozzling devices are fully open. Slight flow losses and small departures from
ideal isentropic flow through the nozzling devices are to be expected, but not to
the extent to which throttling devices are designed to produce flow restrictions.
[0165] Both pressure and enthalpy are transferred to kinetic energy as fluid flows through
a nozzling device. Flow increases to subsonic, sonic, and supersonic velocities depending
on operating conditions and nozzle design as thermodynamic entropy remains substantially
constant. The isentropic nozzling expansion process, with the corresponding drop in
pressure, temperature, and enthalpy, and the increase in velocity is the basis of
non-steady-state refrigeration, heat pump, and air-conditioning cycles.
[0166] The utilization of the high velocity pulsed flows as a means to transfer momentum
and provide flow to thermodynamic fluid within the system is within the scope of this
invention, including but not limited to the incorporation of ejectors and suitably
designed heat exchangers that experience internal recirculation flows as aresult of
the high velocity pulsed flows.
[0167] The scope of the invention is to be determined from the following claims rather than
the foregoing description of certain preferred embodiments.
1. A thermodynamic system wherein a thermodynamic fluid circulates through at least one
heat exchanger with means for providing flow and a pressure rise to the fluid and
a nozzling device which includes a nozzle and a valve automatically fully opened and
closed in a binary fashion for creating accelerated intermittent high velocity bursts
of substantially unrestricted thermodynamic fluid flow through the valve and nozzle
within the system comprising
a) a pulsed ejector having a pulsed ejector suction port into which the thermodynamic
fluid is directed from the nozzle,
b) a pulsed ejector suction conduit connecting the pulsed ejector suction port to
the thermodynamic fluid within the system.
2. A thermodynamic system according to claim 1 the thermodynamic fluid discharged from
the pulsed ejector as combined nozzle flow and pulsed ejector suction port flow creates
internal recirculation flow within the at least one heat exchanger.
3. A thermodynamic system according to claim 1 whereby the thermodynamic fluid reverses
flow direction within the system due to the opening and closing of the nozzling device
valve.
4. A thermodynamic system according to claim 1, including at least one simple pulsed
ejector comprising
a) a simple nozzle in communication with the simple pulsed ejector suction port of
the simple pulsed ejector body,
b) a simple pulsed ejector suction conduit connecting the simple pulsed ejector suction
port to the thermodynamic fluid within the system,
whereby the thermodynamic fluid flow through the system creates suction flow within
the simple pulsed ejector suction port.
5. A thermodynamic system according to claim 4
a) a simple pulsed ejector discharge section communicating combined simple nozzle
flow and simple pulsed ejector suction port flow to the system
whereby the thermodynamic fluid discharged from the simple pulsed ejector as combined
simple nozzle flow and simple pulsed ejector suction port flow creates internal recirculation
flow within the at least one heat exchanger.
6. A thermodynamic system according to claim 4, whereby the thermodynamic fluid reverses
flow direction within the system due to the opening and closing of the nozzling device
valve.
7. A thermodynamic system according to claim 1, wherein
a) the at least one heat exchanger comprises a plurality of substantially vertical
tubes interconnected substantially in parallel by lower and upper headers,
b) when the nozzling device valve is open thermodynamic fluid flow from the nozzling
device and pulsed ejector moves the thermodynamic fluid through the heat exchanger
from the lower to the upper headers so that thermodynamic fluid interacts with substantially
all heat exchange surfaces of the vertical tubes,
c) the pulsed ejector suction conduit recirculates thermodynamic fluid leaving the
upper header of the heat exchanger back to the pulsed ejector when the nozzling device
valve is open.
8. A thermodynamic system according to claim 1, wherein
a) the at least one heat exchanger comprises a plurality of substantially vertical
tubes interconnected substantially in parallel by lower and upper headers,
b) when the nozzling device valve is open thermodynamic fluid flow from the nozzling
device and pulsed ejector moves the thermodynamic fluid through the heat exchanger
from the upper to the lower headers so that thermodynamic fluid interacts with substantially
all heat exchange surfaces of the vertical tubes,
c) the pulsed ejector suction conduit recirculates thermodynamic fluid leaving the
lower header of the heat exchanger back to the pulsed ejector when the nozzling device
valve is open.
9. A thermodynamic system according to claim 2, wherein
a) the at least one heat exchanger comprises a plurality of substantially vertical
tubes interconnected substantially in parallel by lower and upper headers,
b) when the nozzling device valve is open thermodynamic fluid flow through the simple
pulsed ejector moves the thermodynamic fluid through the heat exchanger from the lower
to the upper headers,
c) the simple pulsed ejector suction conduit recirculates thermodynamic fluid leaving
the upper header of the heat exchanger back to the simple pulsed ejector when the
nozzling device valve is open.
10. A thermodynamic system according to claim 2, wherein
a) the at least one heat exchanger comprises a plurality of substantially vertical
tubes interconnected substantially in parallel by lower and upper headers,
b) when the nozzling device valve is open thermodynamic fluid flow through the simple
pulsed ejector moves the thermodynamic fluid through the heat exchanger from the upper
to the lower headers,
c) the pulsed ejector suction conduit recirculates thermodynamic fluid leaving the
upper header of the heat exchanger back to the pulsed ejector when the nozzling device
valve is open.
11. A thermodynamic system according to claim 1 which includes sensing means for sensing
at least one of pressure and temperature of the thermodynamic fluid in said system
to open fully or close the valve in response to a change in at least one of said pressure
and temperature.
12. A thermodynamic system according to claim 11 wherein said sensing means comprises
a thermostatic bulb sensing thermodynamic fluid temperature in the system and a pressure
tap sensing thermodynamic fluid pressure in the system to infinitely vary a setpoint
at which said nozzling device valve opens and closes.
13. A thermodynamic system according to claim 11 wherein momentary temperature and pressure
operating setpoints are relational and the magnitude of the sensed temperature and
the sensed pressure at each moment of system operation varies as the system self-regulates
with changing environment conditions.
14. In a thermodynamic system according to claim 1, means for selectively operating the
system alternatively as a heat pump system comprising
a) reversing valve means for reversing the direction of thermodynamic fluid flow from
a refrigeration mode to a heat pump mode, and
b) the at least one heat exchanger including a condenser and an evaporator, the condenser
in the refrigeration mode functioning as an evaporator in the heat pump mode and the
evaporator in the refrigeration mode functioning as a condenser in the heat pump mode
when said reversal of direction of thermodynamic fluid flow occurs.
15. A thermodynamic system according to claim 14 wherein operation of the system in the
heat pump mode functions to rapidly melt frost accumulated on the evaporator during
operation in the refrigeration mode.
16. A thermodynamic system according to claim 14 wherein the reversing valve means are
provided at the discharge of the compressor and the outlet of the pulsed ejector for
reversing the direction of thermodynamic fluid flow from the refrigeration mode to
the heat pump mode while utilizing a single nozzling device and pulsed ejector.
17. In a thermodynamic system according to claim 14, means for selectively operating the
system alternatively as a heat pump system comprising
a) said nozzling device and pulsed ejector being duplicated as first and second nozzling
devices and pulsed ejectors,
b) said reversing valve means for reversing the direction of thermodynamic fluid flow
from a refrigeration mode to a heat pump mode being without check valves,
c) the first nozzling device and pulsed ejector metering thermodynamic fluid flow
in one direction and the second nozzling device and pulsed ejector metering thermodynamic
fluid flow in the opposite direction, and
d) the condenser in the refrigeration mode functioning as an evaporator in the heat
pump mode and the evaporator in the refrigeration mode functioning as a condenser
in the heat pump mode when the first nozzling device and pulsed ejector cease operation
and the second nozzling device and pulsed ejector meter flow in said opposite direction.
18. A thermodynamic system according to claim 1 wherein by-pass reservoir means are provided
for withdrawing thermodynamic fluid from the system in response to a reduction in
system superheat and returning thermodynamic fluid to the system in response to an
increase in system superheat, whereby as system superheat rises and falls thermodynamic
fluid alternately enters and leaves the reservoir means and alternately enters and
leaves the system.
19. A thermodynamic system according to claim 1 wherein the system is an absorption system
and an absorbent fluid and a refrigerant fluid each circulates in its own flow circuit,
said nozzling device and pulsed ejector being duplicated as an absorber nozzling device
and absorber pulsed ejector and a refrigerant nozzling device and refrigerant pulsed
ejector, and said at least one heat exchanger includes at least one of a refrigerant
evaporator, a refrigerant condenser, and an absorber.
20. A thermodynamic system according to claim 19 wherein refrigerant fluid passes from
the refrigerant evaporator to the absorber pulsed ejector before entering the absorber,
whereby the absorber pulsed ejector is in series with respect to the absorber.
21. A thermodynamic system according to claim 19 wherein the refrigerant fluid circulates
directly from the refrigerant evaporator to the absorber without passing through the
absorber pulsed ejector, whereby the absorber pulsed ejector is in parallel with respect
to the absorber, recirculating thermodynamic fluid from within the system to the absorber.
22. A thermodynamic system according to claim 2 wherein the system is an absorption system
and an absorbent fluid and a refrigerant fluid each circulates in its own flow circuit,
said nozzling device and pulsed ejector being duplicated as an absorber nozzling device
and absorber pulsed ejector and a refrigerant nozzling device and refrigerant pulsed
ejector, and said at least one heat exchanger includes at least one of a refrigerant
evaporator, a refrigerant condenser, and an absorber.
23. A thermodynamic system according to claim 22 wherein refrigerant fluid passes from
the refrigerant evaporator to the absorber pulsed ejector before entering the absorber,
whereby the absorber pulsed ejector is in series with respect to the absorber.
24. A thermodynamic system according to claim 22 wherein the refrigerant fluid circulates
directly from the refrigerant evaporator to the absorber without passing through the
absorber pulsed ejector, whereby the absorber pulsed ejector is in parallel with respect
to the absorber, recirculating thermodynamic fluid from within the system to the absorber.
25. A thermodynamic system wherein a thermodynamic fluid circulates from an evaporator
to a compressor to a condenser and thence back to the evaporator through a nozzling
device which includes a nozzle and a valve automatically fully opened and closed in
a binary fashion to create accelerated intermittent high velocity bursts of substantially
unrestricted thermodynamic fluid flow through the valve and nozzle within the system
comprising
a) a thermostatic bulb sensing thermodynamic fluid temperature in the system, and
b) a pressure tap sensing thermodynamic fluid pressure in the system to infinitely
vary a setpoint at which said nozzling device valve opens and closes.
26. A thermodynamic system wherein a thermodynamic fluid circulates from an evaporator
to a compressor to a condenser and thence back to the evaporator through a nozzling
device which includes a nozzle and a valve automatically fully opened and closed in
a binary fashion to create accelerated intermittent high velocity bursts of substantially
unrestricted thermodynamic fluid flow through the valve and nozzle within the system
comprising
a) the evaporator including a plurality of substantially vertical evaporator tubes
interconnected substantially in parallel by lower and upper evaporator headers, and
b) an evaporator pulsed ejector having an evaporator pulsed ejector port into which
the nozzle thermodynamic fluid flow is directed, an evaporator pulsed ejector suction
port conduit for connecting the evaporator pulsed ejector suction port to the system,
and an evaporator pulsed ejector discharge section for communicating nozzle flow and
pulsed ejector suction port flow to the lower evaporator header, the combined flow
moving thermodynamic fluid upwardly through the evaporator tubes from the lower to
the upper evaporator headers, substantially wetting all the tube heat transfer surface
area,
c) whereby when the nozzling device valve is open pulse thermodynamic fluid flow creates
recirculation flow within the evaporator, and thermodynamic fluid leaving the evaporator
is recirculated to the evaporator by the pulsed evaporator ejector suction conduit
and the pulsed evaporator ejector suction port,
d) whereby as the nozzling device valve opens and closes thermodynamic fluid flow
reverses direction within the evaporator and within the thermodynamic system.
27. A thermodynamic system wherein a thermodynamic fluid circulates from an evaporator
to a compressor to a condenser and thence back to the evaporator through a nozzling
device which includes a nozzle and a valve automatically fully opened and closed in
a binary fashion to create accelerated intermittent high velocity bursts of substantially
unrestricted thermodynamic fluid flow through the valve and nozzle within the system
comprising
a) the condenser including a plurality of substantially vertical condenser tubes interconnected
in parallel by lower and upper condenser headers, and
b) a condenser ejector having a condenser ejector suction port, a condenser ejector
suction conduit, and a condenser ejector discharge section for directing thermodynamic
fluid vapor from the compressor upwardly through the condenser tubes from the lower
to the upper condenser headers,
c) whereby when the nozzling device valve is open carrying the thermodynamic fluid
upwardly through the condenser tubes from the lower to the upper condenser headers
so that thermodynamic fluid liquid condenses on inner surfaces of the condenser tubes
and flows downwardly in counterflow relation to thermodynamic fluid vapor carried
upwardly through the condenser tubes, and thermodynamic fluid is recirculated from
the upper condenser header to the lower condenser header by the condenser ejector
suction conduit and the condenser ejector suction port,
d) whereby as the nozzling device valve opens and closes thermodynamic fluid flow
reverses direction within the condenser and within the thermodynamic system.
28. A thermodynamic system according to claim 27 wherein the upper condenser header is
a dead-end header.
29. In a thermodynamic process wherein a heat exchange fluid is circulated, a method of
continual thermodynamic efficiency self-optimization in real time as energy is exchanged
in the process with an external environment which comprises
a) directing the heat exchange fluid through a valve and nozzle,
b) sensing the pressure of the heat exchange fluid in the system,
c) sensing the temperature of the heat exchange fluid in the system,
d) converting the sensed temperature to an equivalent sensed pressure, and
e) automatically opening fully or closing the valve in a binary fashion in response
to a change in the relation between the sensed pressure and the sensed temperature
thus permitting substantially unrestricted bursts of fluid flow through the valve
and permitting acceleration of the intermittent bursts of fluid flow by the nozzle.
30. A method according to claim 29 wherein the opening and closing of the valve functions
in a mechanical feedback loop utilizing internal pressure information and internal
temperature information to self-regulate said opening and closing of the valve and
flow through the nozzle.
31. A method according to claim 30 wherein the opening and closing of the valve permits
pulses of fluid flow through the thermodynamic system which creates recirculation
flow within the thermodynamic system heat exchangers and causes the thermodynamic
fluid to reverse flow direction within the thermodynamic system.