1. Background of the invention
[0001] This invention is directed to a cryogenic system wherein both the compressor and
expander, which operate with the cryogenic refrigerant fluid in the system, are rotary
screw type machinery of the Lysholm type.
[0002] Lysholm built an early prototype of the rotary screw compressor in 1934. Some of
his development work was described in the Proceedings of the Institution of Mechanical
Engineers, Vol. 150, No.1, Pages 11-16 and 4 plates 1943. One of the main features
of this screw compressor is the fact that it can run without oil or other lubricant
in the compression chamber. No oil is necessary because the rotors do not contact
each other or the casing. The only mechanical contact is in the bearings and in the
timing gears which can be located on the outside of the casing and away from the refrigerant
gas flow stream. The Lysholm type rotary screw compressor has two rotors with intermeshing
lobes. Within the intermesh of the lobes and housing, the compression takes place.
Two helical rotors comprise the working . parts of the screw compressor. The male
rotor generally has four lobes and rotates 50 percent faster than the female rotor
which has six flutes between which are grooves in which the lobes interengage. Other
ratios of lobes to flutes are also used. The gas is compressed in the spaces between
the housing, the lobes and the grooves. The lobes and the grooves are helical so that
the space appears to move progressively toward the outlet end of the housing, and
the space becomes progressively smaller along the length of the rotors as the rotors
rotate. Thus, gas taken in the inlet port at the suction end is compressed in the
space as the rotors turn and it is finally delivered at higher pressure from the outlet
port at the delivery end of the housing. The inlet and outlet ports are automatically
covered and uncovered by the shaped ends of the rotors as they turn.
[0003] There has been considerable development work done on the improvement of such screw
compressors. Most of the patents are owned by Svenska Rotor Maskiner which devoted
the pioneer effort in this art and appears to hold most of the patents. The company
is located in Nacka, Sweden.
[0004] Nilsson, U.S. Patent 3,245,612 and Schibbye, U.S.Patents 3,283,996 and 3,423,01?
are particularly directed to the shapes of the lands and the grooves in the rotors,
but show the porting and general organization of the rotary screw compressor to show
how compression and expansion are achieved in such a structure. Furthermore, this
type of screw compressor is illustrated as being the compressor in refrigerator systems
in U.S.Patents 3,432,089; 3,811,291; 3,848,422 and 3,945,216. While the use of screw
compressors has been recognized for refrigerator compressor service, the use of such
devices as expanders has not been recognized. Furthermore it has not been previously
recognized that screw compressors and expanders in the same refrigerator can efficiently
run at about the same speed so that they can be coupled directly or through gearing,
for speed control of the expander and for power feedback from the expander. In the
refrigeration arts, it is known that it is necessary to extract work during expansion
to produce refrigeration, with some refrigerant gases within some of their operating
temperature ranges. In the past, piston expanders have been used, usually in smaller
refrigerators, and turbo expanders have been used, usually in larger refrigerators.
While the work output of such expanders is not significant in terms of total refrigerator
input power, speed control of the expander is necessary. Such speed control has been
difficult where the turbo expander runs at very high speed. It is part of this invention
that the employment of an expander coupled to and running with the compressor is feasible
when screw-type equipment is used for refrigerant gas compression and expansion. This
arrangement has not previously been used in refrigerators and results in equipment
which is of considerably longer life so that it can be employed in locations where
maintenance is impractical. Furthermore, the system is of low weight to unit of refrigeration
in modest sizes, and is of low power requirement per unit of refrigeration in the
same modest sizes. Therefore, such a refrigerator system can be used to cool devices
for a long maintenance-free life, and can be employed in locations where total weight
and input power should be minimized.
2. Summary of the invention
[0005] In order to aid in the understanding ofthis invention, it can be stated in essentially
summary form that it is directed to a screw compressor-expander refrigeration system
wherein a screw compressor compresses a refrigerant gas,which is cooled by heat exchange
and delivered to a screw expander which expands the refrigerant gas for the cooling
thereof, with the expander being coupled to the compressor to feed work to the compressor
and regulate expander speed, so that refrigeration is achieved.
[0006] It is thus an object of this invention to provide a screw compressor-expander cryogenic
system wherein Lysholm-type gas handling equipment is used for compression and expansion
of the gas to produce refrigeration. It is another object of this invention to provide
a refrigerator wherein a long trouble-free life isachieved. It is a further object
to provide a screw-compressor-expander cryogenic refrigerator system wherein the expander
runs at the same relative- rotative rate as the compressor to permit coupling between
the expander and compressor for speed control of the expander and feedback of work
from the expander to the compressor. It is another object to provide a screw compressor-expander
cryogenic refrigerator system wherein the employment of a screw-type compressor and
a screw-type expander permits the production of refrigeration at an increased value
of unit of refrigeration per unit of weight so that the system can be employed in
locations where weight is critical. It is a further object to provide a cryogenic
refrigerator system which employs a screw-type compressor and a screw-type expander
wherein more refrigeration is produced per unit of input power to permit use of the
refrigerator system in locations where power must be conserved.
[0007] Other objects and advantages of this invention will become apparent from a study
of the following portion of the specification, the claims and the attached drawings.
Brief description of the drawings
[0008] In the accompanying drawings:
Figure 1 is a perspective view of the screw compressor-expander structure, with parts
broken away to show a portion of the internal mechanism;
Figures 2 and 3, when taken together, comprise a longitudinal section through the
screw compressor-expander mechanism, with some parts broken away and some parts taken
in section;
Figure 4 is an enlarged detail of the seal structure, with parts broken away and parts
taken in section;
Figure 5 is a perspective view with parts broken away and parts taken in section of
the bearing and seal structure at the end of the expander shaft;
Figure 6 is a plan view, with parts broken away and parts taken in section of the
screw compressor-expander structure, shown in conjunction with its associated system
components so that the cryogenic refrigeration system is shown.
Figure ? is a temperature-entropy diagram showing the operating conditions of the
cryogenic system.
Description of the preferred embodiment
[0009] Referring particularly to Figs. 1, 2, 3, and 6, a screw compressor-expander mechanism
is generally indicated at 10. The mechanism 10 is used in conjunction with an external
refrigerant circuit 12, see Fig.6, to result in the screw compressor-expander cryogenic
system of this invention. The mechanism 10 broadly comprises a motor 14 which drives
a compressor 16 and which is also coupled to an expander 18.
[0010] The motor 14 comprises a motor housing 20 within which is mounted the electrical
windings .and the rotor of the motor 14. Fig.6 shows a power supply 21 connected to
the motor 14 for supplying the requisite electric power thereto. The supply 21 may
include a.source, such as a solar array, and a power conditioning system when the
refrigerator 10 is deployed in space. Power supply 21 may be a more conventional power
line, generator or battery when the refrigerator 10 is used on ground, air, or shipboard
equipment. A shaft 22 extends from the housing 20 on its right end. The shaft 22 is
mounted on a pair of antifriction bearings 24 and 26, on the ends thereof, for the
rotary support of the rotary portions of the motor. The ball bearings 24 and 26 are
mounted in a pair of respective bosses 28 and 30, and the bosses are mounted on the
motor housing..A cover 32 encloses the exterior of the bearing 24 and the boss 28.
An oil inlet connection 34 furnishes oil to the bearing 24 while an oil outlet connection
36 returns the oil from the interior of the cover 32 for recirculation. A seal 38
prevents the entrance of oil from the region of the bearing 24 into the interior of
the motor housing 20. A cover 40 protects the exterior of the motor housing and the
bearing assembly of which the bearing 24 is a part. An oil tube 42 may be wrapped
around the motor housing 20, or oil passages may be provided within the exterior structure
of the motor housing 20 to provide for coolant flow to carry away the heat of the
motor 14. Oil tube 42 is part of the general lubrication system of the mechanism 10,
and it may be the tube which supplies the oil inlet connection 34. Cover 40 protects
the exterior of the motor housing 20, the cooling oil tube 42, and the bearing structure
under the cover 32.
[0011] The shaft 22 extends out of the boss 30 and beyond the bearing 26 and has an interior
spline 44. A housing 46 surrounds the boss 30 and has an interior boss 48 therein.
The boss 48 has a shaft 50 therein in alignment with shaft 22 and a shaft 52 therein
oriented in parallel to the shaft 50. The shafts 50 and 52 are respectively supported
on a bearing 54 and.a bearing 56. A seal 58 is located around the shaft 50 interiorly
and adjacent to the bearing 54 while a seal 60 is positioned around the shaft 52 and
adjacent the bearing 56.
[0012] A timing gear 62 is mounted on the shaft 50 while a timing gear 64 is mounted on
the shaft 52. The timing gear 62 is the drive gear and it engages the timing gear
64 which is the driven gear. The shaft 50 has an exterior spine 66 adjacent the gear
62 and extending into and engaging the spine 44. By this construction, with rotation
of the motor shaft 22, the shafts 50 and 52 also rotate. Oil is supplied within the
housing 46 to lubricate the bearings 26, 54 and 56. The oil also lubricates the spline
coupling defined by the splines 44 and 66, as well as lubricates the mesh of the gears
62 and 64. Furthermore, the housing 46 serves as the oil sump and interiorly thereof
is located the oil pump 68 which takes suction through an appropriate suction line
from the oil within the sump. The suction line 70 and the oil pump 68 are specifically
designed to pump in accordance with the local ambient conditions. In normal gravitational
environments, the suction may be a filter in the bottom of the sump (from a gravitational
viewpoint) while in non- gravitational or very low gravitational requirement, the
pump suction may be especially designed to pick up globules of oil floating free within
the housing, and/or suction may pick up oil which is moving by surface tension on
the inside of the walls of the housing 46. In another manner of operation the housing
46 may be completely filled with oil so the pump 68 operates like in gravitational
conditions. The oil pump 68 delivers oil to the various needs of the mechanism 10,
including the lubrication of the bearing 24 and the cooling of the motor 20. There
are other lubricant requirements in the mechanism 10, described hereinafter, and these
are also supplied by the pump 68. A connection 74 and a connection 76 are through
flow connections for the housing 46. The oil discharge from the pump 68 may be cooled
as in a cooler 78 illustrated in Fig.1. The various connections illustrated on the
cooler 78 illustrate connections for the utilization of oil from the cooler.
[0013] A compressor housing 80 houses a lobed screw compressor rotor 82 on shaft 50 and
a mating recessed rotor 84 on the shaft 52. The rotors 82 and 84 closely interfit
with each other, and closely interfit with the casing 80 both radially and at the
ends. The housing 80 has an opening on the side of the housing 80 adjacent the intermesh
of the rotors at one end thereof to define an inlet zone 86 to which is connected
a suction line 88, see Fig.6. At the other end of the housing 80, also at the intermesh
between the rotors 82 and 84 is an outlet zone 90 to which is connected an outlet
line 92.
[0014] The right hand ends of the shafts 50 and 52 are rotatably supported in a set of anti-friction
bearings 94 and 96 respectively which are in turn protected by seals 98 and 100 respectively.
The inlet and outlet ports in association with the inlet and outlet zones 86 and 90
are disclosed in several of the patents discussed in the background. The shapes of
the rotors 82 and 84, in connection with the inlet and outlet ports and the compressor
housing 80 are such that compression is achieved in the space between the rotors and
the end of the housing 80. As the rotors rotate, individual spaces defined by the
lobes and recesses of the rotors appear to proceed along in the housing. In the present
case, rotation is such that the procession appears to be from left to right. As the
inlet port in the left end of the housing 80 is cut off, the volume of the space appears
to decrease so that compression takes place. When compression reaches the desired
value,then the outlet port is uncovered to discharge the compressed gas to the outlet
line 92.
[0015] A cooling chamber 102 may embrace the high pressure end of the compressor housing
80 to remove some of the heat of compression, if required to maintain reasonable temperature
gradients and limits in the housing, rotors and appurtenant structure. The cooling
chamber 102 may be supplied with circulating oil as a coolant, or may employ another
coolant, as desired.
[0016] A housing 104 is flanged to the right end of the compressor housing 80. The housing
104 contains a pair of expander shafts 106 and 108 which are mounted on a pair of
bearings 110 and 112 and which are sealed by a pair of seals 114 and 116. A pair of
timing gears 118 and 120 are respectively mounted on the shafts 106 and 108. The timing
gears interengage to maintain the shafts at particular interrelated angular positions
and angular rate ratios. The shaft 106 is coupled to the shaft 50 by means of spline
coupling 122 so that the shaft 106 turns with the shaft 50, and the shaft 108 turns
with the shaft 106.
[0017] While the preferred embodiment incorporates the direct coupling between the expander
18 and the compressor 16, as exemplified by the spline coupling 122, it can also be
appreciated that other relationships are possible. For example, the expander can be
placed close to the refrigeration load while the compressor 16 may be located conveniently
to the source of power and/or a location where the heat of compression can be rejected.
In such a case, ambient refrigeration gas is piped to and from the compressor to the
location of the expander 18. The cryogenic heat exchanger between inlet and outlet
expander gas would be located close to the expander. In the case where the expander
is remotely located, speed control of the expander would be achieved by a separate
motor/generator directly or gear coupled to the expander shaft 106. Furthermore, in
such an arrangement the expander canrun at a higher speed than the compressor. A higher
speed is feasible because the expander 18 is smaller in physical size than the compressor
16.
[0018] The shafts 106 and 108 are tubular and extend into an expander housing 124. A lobed
rotor 126 is mounted on the shaft 106 while a rotor 128 having mating recesses thereon
is mounted on the shaft 108. The lobes and recesses of the rotors 126 and 128 intermate
and define spaces which act to expand gas. They are of the same nature as the compressor
rotors in that the expansion takes place in the spaces between the housing 124 and
the rotors 126 and 128. The criteria for the construction of this expander is the
same as for the Lysholm type compressors discussed above, except that the structure
runs in the opposite direction. As seen in Fig.6, an inlet line 130 is connected to
the inlet port of the expander 18 while an outlet line 132 is connected to the outlet
port of expander 18.
[0019] The expander housing 124 is mounted on tubular supports, such as a tubular support
134 seen in Fig.3 which is mounted on the housing 104. The support 134 is in supporting
engagement with the expander housing 124. A tubular support 136 extends between the
expander housing 124 and a bearing housing. 138. A dewar housing 140 encloses the
expander 18 and mounts on the housing 124. The dewar housing 140 insulates the expander
18 which operates at cryogenic temperatures. Furthermore, bearing housing 130 is mounted
on the outer end of the dewar housing 140. The hollow shafts 106 and 108 extend through
the rotors and are rotatably supported in the bearing housing 138 in a pair of bearings
142 and 144, see Figs. 3 and 5. The bearings 142 and 144 are respectively protected
by a seal 146 and a seal 148. Lubricant is supplied and drained from the bearings
142 and 144 by means of an oil inlet 147 and an oil outlet 149. These provisions for
oiling permit the circulation of oil from the oil pump 68 through the bearing area
and out therefrom. Since the expander 18 is cold, the oil may supply heat to the bearings
142 and 144 to keep them temperature stabilized.
[0020] The shafts 106 and 108 are hollowed tubes to limit heat transfer to the physical
structure of the expander from the region of the bearings. However,in order to keep
the seals 114, 116, 146, and 148 as well as the bearings 110, 112, 142, and 144 temperature
stabilized, thermal plugs are fitted into the shafts at the ends inside the bearings
and the seals. A thermal plug 150 is illustrated as being within the shaft 106 interiorly
of the bearing 110 and the seal 114, while a thermal plug 152 is illustrated as being
in the interior of the tubular end of the shaft 106 interiorly of the bearing 142
and the seal 146. In addition, a sleeve 154 is fitted exteriorly of the shaft 106
within the seal 114 while a sleeve 156 is fitted exteriorly of the shaft 106 interiorly
of seal.146.These sleeves are fitted throughout, within the seals, as for example
the sleeve 158 fitted exteriorly of the shaft 50 within the seal 98.
[0021] Fig. 4 illustrates the seal 98 in more detail. The shaft 50 has the sleeve 158 positioned
on its exterior. The sleeve 158 is of magnetizable material and acts as a pole-piece,
and is necessary when the shaft 50 is of non-magnetic material. In cases where the
shaft 50 is of magnetizable material, the sleeve 158 is not required. A bushing 160
in the form of a tubular cylinder which is axially magnetized is provided around the
sleeve 158. The bushing 160 is a permanent magnet but a solenoid coil could be substituted.
A magnetic pole piece 162 is positioned at one end of the magnetic bushing 160 and
a magnetic pole piece 164 is positioned at the other end of the magnet bushing 160.
The pole pieces are in the form of rings and are sealed within a bore 166 in the housing
80 by means of an 0-ring 168 and an 0-ring 170 respectively. The pole pieces 162 and
164 have annular grooves therein such as a groove 172 in the pole piece 162 and a
groove 174 in the pole piece 164. These grooves concentrate the magnetic field in
the radial space between the pole pieces and the sleeve 158. The lubricant supplied
to the bearing 94 is of oily-type material. It may be of hydrocarbon base or silicone
base, so that it supplies the lubricant at an acceptable viscosity over the operating
range of the mechanism 10. Furthermore, very finely divided magnetizable iron particles
are present in the lubricant supply. These iron particles are sufficiently small to
pass through any filters in the lubrication system and are small enough that they
do not reduce the life of the anti-friction bearings. The lubricant can circulate
through the bearings, as through the bearing 94 and reach the annular space between
the pole piece 164 and the sleeve 158. A magnetizable particle diameter in the rangeof
50 to 100 Angstroms is satisfactory in this work. There is sufficient magnetizable
material such as iron powder in the oil lubricant so that when the iron is trapped
between the pole pieces 162 and 164 and the sleeve 158, no oil passes. Thus,this provides
a noncontacting long life seal. A hard packing 178 is provided between the sleeve
158 and the end of the bore 166 to minimize heat transfer from the compressed gas
to the seal area.
[0022] A plurality of axially oriented cooling holes are drilled into the shaft 50 from
the end underneath the bearing, all the way underneath the seal. A hole 180 is shown
in Fig.4, and is exemplary of several such holes drilled parallel to the axis, and
positioned off axis just under sleeve 158. These cooling holes permit the circulation
of oil into the region beneath the seal 98 to carry heat away from the seal area to
maintain seal temperatures.
[0023] Referring to Figs. 6 and 7, the cycle parameters are described. The system operates
in an environment in which the mechanism 10 is generally at about 300° K, when in
equilibrium with the ambient. In a specific cycle example, the compressor suction
line 88 is at 199° K and 1/2 atmosphere absolute. See point 1 in Fig. 7. The refrigerant
gas is nitrogen in the present operating cycle example, but.may be nitrogen, argon,
helium or neon depending on the desired refrigeration temperature.. The screw compressor
16 is driven by the motor 14 with the lobed rotor 82 running about 10,000 REM. In
this example the rotor 82 has 4 lobes while the rotor 84 has 5 recesses. The screw
compressor 16 is such as to raise the pressure in the outlet line 92 to 1 atmosphere
at point 2 in Fig.?. A heat exchanger 184 rejects heat to the ambient, as by fluid
circulating in the circulating line 186. The circulating line 186 may carry a liquid
or a gas, or in space applications may directly radiate heat to space. In the heat
exchanger 184, heat is rejected from the refrigerant gas so that in the line 188 the
conditions are as at point 3 in Fig.?. Temperature is at 300°K.
[0024] A heat exchanger 190 is a counterflow heat exchanger with heat exchange between the
fluid in line 188 and the refrigerant fluid flowing to the compressor in suction line
88. In the heat exchanger 190, the refrigerant gas is cooled from point 3 to point
4 in the TS diagram of Fig. 7. The fluid flows from the heat exchanger into expander
inlet line 130. At that point, the refrigerant gas is at 185° K.
[0025] The expander 18 in the present example is running at the same speed as the compressor,
because the lobed rotor 126 thereof is running at the same speed as the lobed rotor
82 of the compressor 16. It is understood that if desired, a gear box may be employed
within the housing 104 so that the expander may run at a different speed. However,
the present preferred embodiment is to have the two shafts run at the same speed,
in view of the mechanical simplicity. There is not believed to be a sufficient thermodynamic
advantage to operate at a different speed to warrant the additional complexity caused
by the gear connection. In either a direct drive situation as illustrated in Fig.3,
or in a gear drive, the expander rotors are coupled to the compressor rotors which
in turn are controlled inspeed by the drive motor 14. This has the effect of controlling
the speed of the expander 18 as well as feeding back to the compressor power resulting
from the gas expansion. In the expander, the refrigerant gas is expanded to the suction
pressure of one half atmosphere and to 177°K, at point 5. This is the condition in
the outlet line 132. In same conditions, the refrigerant may be a mixed vapor-liquid
fluid at the expander outlet. The screw expander 10 can handle such a mixed fluid
without damage. A refrigeration load 192 supplies heat to the refrigerant gas. It
is here that the useful refrigeration is achieved. A refrigerator heat load 193 is
illustrated in Fig.6 as delivering heat at below ambient temperatures to the refrigeration
load heat exchanger 192. The refrigeration load 193 is equipment which requires a
subambient temperature for proper operation. It may be an electronic device such as
a cooled amplifier. It may be a sensor such as an infrared.sensor which requires cooling
to reduce background electronic noise signals. It may even be a compartment in which
materials can be stored or treated while at subambient temperatures. The refrigeration
temperature is about 180
0K, with 177
0K gas going into the refrigeration load and 184
0X gas coming out of the refrigeration load in a line 194. The conditions in line 194
are represented at point 6 in Fig.7 and represent the cold input to the heat eschanger
190. Fluid in the line 194 passes through the heat exchange 190 to the line 88 and
exchanges heat therein. This closes the cycle. The above are calculated values.
[0026] The dewar housing 140 is insulated in order to maintain the expander 18 in a cool
condition, with a minimum amount of heat conducted and radiated into the expander.
The refrigeration heat load 192 is schematically shown exteriorly to the dewar 140
in Fig.6, but may be interiorly thereof, as an infrared radiation detector, or other
refrigeration load.
[0027] The mass flow rate of the system depends upon the gas, the amount of cooling desired
and the refrigeration temperature. The compressor rotor 82 and the expander rotor
126 are sized to handle the mass flow rate. The working pressure increase in the compressor
is one half atmosphere. In a medium size machine, the compressor rotor 82 runs at
10,000 RPM.
[0028] Compared to Stirling cycle machines and Vuilleumeir machines, the present system
has a favorable specific power consumption and has a better chance to reach maintenance-free
life of up to ten years, and accordingly is particularly useful.
[0029] This invention having been described in its preferred embodiment, it is clear that
it is susceptible to numerous modifications and embodiments within the ability of
those skilled in the art and without the exercise of the inventive faculty. Accordingly,
the scope of this invention is defined by the scope of the following claims.
1. A refrigerator system comprising a screw compressor having a housing having inlet
and outlet ends, an inlet and an outlet adjacent the ends of said compressor housing;
first and second rotors rotatably mounted within said housing, said first and second
rotors respectively having intermeshing lobes and recesses configured so that compression
occurs in gas passing through said compressor; an expander having an expander housing
having inlet and outlet ends, an inlet adjacent one end of said expander housing and
an outlet on the other end of said expander housing; first and second expander rotors
rotatably mounted within said expander housing, said first and second rotors respectively
having intermeshing lobes and recesses so that gas expansion takes place upon rotation
of said expander rotors in said expander housing; and means interconnecting said inlet
and outlet on said compressor housing and said inlet and said outlet on said expander
housing for producing refrigeration upon rotation of said rotors.
2. The refrigerator system of claim 1, wherein a motor is connected to said compressor
to drive said compressor rotors in said compressor housing.
3. The refrigerator system of claim 1 or 2 wherein said first and second compressor
rotors have a gear coupling therebetween so as to regulate relative angular position
of said first and second compressor rotors.
4. The refrigerator system of claim 3 wherein said first and second compressor rotors
are respectively mounted on shafts, said shafts extending exteriorly of said compressor
housing, first and second gears respectively mounted on said first and second shafts,
said first and second gears interengaging so that said first and second compressor
rotors are maintained in a predetermined angular relationship.
5. The refrigerator system of any one of claims 1 to 4 wherein said first and second
compressor rotors are in a chamber in said compressor housing and/or said first and
second expander rotors are in a chamber in said expander housing, each of said rotors
being mounted on a shaft, a bearing interengaged between each of said shafts and the
respective housing, said bearings being positioned exteriorly of said chambers.
6. The refrigerator system of claim 5 wherein a seal is positioned between the bearing
on each said shaftand the corresponding chamber.
7. The refrigerator system of claim 6 wherein said seals have means for providing
a magnetic field therein, and lubrication means is providedfor said bearings for lubricating
said bearings with a lubricant fluid having magnetizable properties so that each said
magnetic seal prevents the magnetizable lubricant from entering said chambers.
8. The refrigerator system of claim 7 wherein said seals comprise a portion of each
said seal rotating with said shaft and a portion of each said seal fixed with respect
to said housing, one of said portions being a magnetic flux path and the other of
said portions being a magnet so that when a magnetizable lubricant liquid is used
to lubricate said bearing, the magnetizable lubricant liquid is prevented from passing
into said compressor housing past said magnetic seal.
9. The refrigerator system of claim 8 wherein said lubricant is a mixture of finely
divided solid magnetizable material in a viscous liquid lubricant.
10. The refrigerator system of any one of claims 1 to 9 wherein said expander rotors
have a gear interconnecting therebetween so that said first and second expander rotors
rotate at a predetermined relative angular velocity.
11. The refrigerator system of any one of claims 1 to 10 wherein said expander is
rotatively coupled to said compressor to control expander speed and transmit power
therebetween.
12. The refrigerator system of claim 11 wherein said first compressor rotor is positively
coupled to said first expander rotor so that said first compressor rotor and said
first expander rotator operate at a fixed angular rotation rate ratio.
13. The refrigerator system of claim 12 wherein the ratio is 1 to 1.
14. The refrigerator system of claim 13 wherein said first compressor rotor and said
first expander rotator are axially aligned and are rotationally positively coupled.
15. The refrigerator system of any one of claim 1 to 14 further including a refrigeration
load thermally connected to said expander outlet so that said refrigeration load delivers
heat to the gas in said refrigeration system so that said refrigeration load is cooled.
16. The refrigerator system of any one of claims 1 to 15 wherein said outlet of said
compressor is connected to means for rejecting heat from refrigerant gas, and said
means is connected to a counterflow heat exchanger and said counterflow heat exchanger
is connected to deliver gas to the inlet of said expander, said expander outlet being
connected to means for receiving heat from a refrigeration load for cooling the refrigeration
load, and said means for receiving heat being connected through said counterflow heat
exchanger to said compressor inlet so that a closed cycle gas refrigeration system
is achieved.
17. The refrigerator system of claim 16 further including a device to be refrigerated,
said device to be refrigerated being thermally connected to said means for receiving
heat from a refrigeration load; and an electric motor is connected to said compressor
to drive said compressor and an electric power supply is connected to said compressor
motor to energize said compressor motor.