Background of the Invention
[0001] This invention relates generally to ventilation systems. More particularly, the invention
relates to terminals for diffusing and distributing air from a ventilation supply
duct into a space such as a room.
[0002] Ventilation systems are widely used to distribute air within enclosed spaces such
as rooms in buildings or ships, or cabins of motor vehicles or aircraft. The distributed
air may be heated, cooled, dehumidified, filtered or otherwise conditioned or purified
by specialized equipment adapted to the purpose. Common to nearly all ventilation
systems are terminals at the outlet ends of the ducts supplying air to the space or
spaces to be ventilated.
[0003] A terminal serves several functions. One is to distribute the air exiting the terminal
as widely as possible in order to minimize the number of duct terminals required to
serve a given space. Another is to mix the air exiting the terminal with air already
in the space so as to promote uniform distribution of air having a desired condition
(
e.g. temperature, humidity) within the space and thus to prevent drafts and "dead," hot
or cold areas. The terminal should contribute as little as possible to system pressure
losses and also as little as possible to system radiated noise.
[0004] Many prior art ventilation terminals attempt to achieve their design objectives by
diffusing the air stream from the supply duct through the terminal to an outlet having
a much greater area than that of the duct and by turning the airstream at the outlet
into one or more directions by an arrangement of deflectors, baffles or vanes. The
losses through such a terminal can be large because the relatively large spreading
or diffusion angle causes separated air flow at the inner surface of the diffuser
section of the terminal (a condition known as diffuser stall), with a resultant energy
dissipation in turbulence. Stall at the inner surface of the diffuser also reduces
air flow through that region and results in a high velocity jet at the center of the
terminal air flow passage. The high velocity jet has embedded turbulence from the
diffuser stall. This high velocity jet generates high noise levels when it passes
through and impinges on the exit deflectors. Because of the relatively high pressure
loss through such a terminal, the ventilation system fan or fans must operate at a
higher loading to achieve desired air flow rates and thus the fans produce greater
noise levels than if the terminal were not in the system.
[0005] At least one prior art ventilation air terminal,
see Kurth
et al., U.S. Patent 2,825,274 issued 4 March 1958, has an ejector that induces air from
the spaces served by the terminal to mix with the flow of conditioned air from the
air supply duct. But, while the '274 terminal is an improvement over terminals without
an ejector, standard ejectors (without lobes) do not operate effectively within the
constraints of the short mixing length of a ventilation terminal and therefore increase
the pressure loss through the terminal. The stream of air entering the terminal and
the stream of mixed air exiting the terminal are in close proximity, leading to re-ingestion
or "short circuiting" of the mixed air and therefore reducing the mixing and coverage
effectiveness of the terminal.
Summary of the Invention
[0006] The present invention is a ventilation air terminal incorporating a mixer ejector.
The terminal offers improved mixing, reduced pressure loss and reduced radiated noise.
[0007] The terminal delivers air from an upstream supply duct through a primary flow passage
in the terminal to an outlet. One boundary of the primary flow passage is a lobed
array. The lobed array has a plurality of lobes aligned longitudinally along the array.
The height of the lobes increases gradually in an upstream to downstream direction
along the array. On the other side of the lobed array is an ejector flow passage.
The configuration of the lobes is such that a lobe in one flow passage is a trough
in the other flow passage. Viewed from downstream, the lobes have a wave-like appearance.
The ejector flow passage conducts air from a recirculating air inlet to the outlet
of the terminal. The lobes produce streamline vortices and other stirring mechanisms
thus producing rapid mixing with low losses. This mixing interaction between the air
flow in the primary flow passage as the air passes through the lobed array and the
air in the ejector flow passage causes air to flow in the ejector flow passage from
the recirculating air inlet to the air outlet. The mixing interaction also causes
the recirculating air to mix with the primary air that is discharged from the terminal.
The terminal draws air from the space it serves and mixes this recirculated air with
the supply air before discharging the mixed airstreams to the space. The terminal
thus reduces any large variation in condition,
e.g. temperature, between the supply air and the ambient air within the space so that
unpleasant drafts as well as hot or cold spots are reduced. The mixing action also
serves to reduce the total velocity of the air exiting the terminal into the space
with a resultant reduction in air flow noise produced by the terminal.
[0008] One may configure the terminal of the present invention in more than one embodiment,
such as one discharging along the same line as the direction of flow through the supply
duct, or in which the discharge airstream is at some other angle.
Brief Description of the Drawings
[0009] The accompanying drawings form a part of the specification. Throughout the drawings,
like reference numbers identify like elements.
[0010] FIG. 1 is an isometric view, partially broken away, of one embodiment of the terminal of
the present invention.
[0011] FIG. 2 is a top plan view, partially broken away, of the terminal depicted in
FIG. 1.
[0012] FIG. 3 is a sectioned, through line
III-III in
FIG. 2, elevation view of the terminal depicted in
FIG. 1.
[0013] FIG. 4 is a second isometric view of the terminal depicted in
FIG. 1.
[0014] FIG. 5 is a sectioned, through line
V-V in
FIG. 2, elevation view of the terminal depicted in
FIG. 1.
[0015] FIG. 6 is a schematic diagram showing air flow through the terminal depicted in
FIG. 1.
[0016] FIG. 7 is an isometric view of another embodiment of the terminal of the present invention.
[0017] FIG. 8 is a bottom plan view of the terminal depicted in
FIG. 7.
[0018] FIG. 9 is a sectioned, through line
IX-IX in
FIG. 7, of the terminal depicted in
FIG. 7.
[0019] FIG. 9 is a sectioned, through line
VII-VII in
FIG. 7, eleva tion view of the terminal depicted in
FIG.
7.
[0020] FIG. 10 is a schematic diagram showing air flow through the terminal depicted in
FIG. 7.
Description of the Preferred Embodiments
[0021] FIGS. 1 through
5 depict one embodiment of the terminal of the present invention.
FIG. 1 is an isometric view, partially broken away,
FIG. 2 is a top plan view, partially broken away,
FIG. 3 is a sectioned side elevation view,
FIG. 4 is an isometric view from another angle and
FIG. 5 is a sectioned elevation view of a portion of the terminal. In this embodiment, a
ventilation terminal discharges air from a ventilation duct into a space at right
angles to the direction of the inlet air. A terminal of this configuration would be
appropriate where flush mounting with a surface such as a ceiling is not required
or desired.
FIGS. 1 through
5 show ventilation terminal
10, the major components of which are inlet duct
13, terminal casing
14, baffle plate
15 and lobed array
22.
[0022] Air from an upstream air supply duct (not shown) enters inlet duct
13 of terminal
10 through air inlet
11. All of the air entering terminal
10 through air inlet
11 (primary air) must flow through primary flow passage
31, which is formed and defined by terminal casing
14 and lobed array
22, before exiting terminal
10 through air outlet
12. Air from the space served by terminal
10 (recirculating air) can enter the terminal through recirculating air inlet
33 in baffle plate
15. To exit through air outlet
12, recirculating air entering terminal
10 through recirculating air inlet
33 must pass through ejector flow passage
32. Ejector flow passage
32 is formed by and between baffle
15 and lobed array
22.
[0023] Lobed array
22 has a plurality of radially arranged lobes
23 aligned so that they conform longitudinally to the stream of primary air flowing
from inlet duct
13 to air outlet
12 through primary air passage
31. Lobes
23 penetrate alternately into both primary flow passage
31 and ejector flow passage
32 so that a lobe in one of the passages is a trough in the other. The height of lobes
23 increases gradually in an upstream to a downstream direction along the array. When
viewed from downstream (
FIG. 5), lobes
23 have a wave-like appearance. Taken together, lobed array
22, primary flow passage
31 and ejector air passage
32 form a mixer ejector.
[0024] FIG. 6 shows schematically the operation of terminal
10. Primary air enters terminal
10 through air inlet
11. As the primary air passes through terminal
10 it turns and passes through the lobes and troughs of lobed array
22 in primary flow passage
31. Ejector mixing interaction between the air flow in primary air passage
31 and the air in ejector air passage
32 causes a flow of air in passage
32 from recirculating air inlet
33 to air outlet
12, causing air from the space served by terminal
10 to be drawn into the terminal and mixed with the primary air stream from the ventilation
supply duct.
[0025] The configuration of air outlet
12 is that of a diffuser, lowering the static pressure at the outlet and thus increasing
the secondary air flow through terminal
10. Terminal
10 does not require a diffuser but, in addition to lowering the static pressure, the
diffuser improves the secondary air pumping power of terminal
10. This is because vortices generated in the primary and secondary air streams by lobes
23 energize the diffuser boundary layer and allow relatively large diffuser angles without
stalling. The absence of stall means that the full energy of the primary air stream
is available to pump the secondary air stream (with about 90 to 95 percent efficiency).
[0026] FIGS. 7 through
9 depict another embodiment of the terminal of the present invention.
FIG. 7 is an isometric view, partially broken away,
FIG. 8 is a bottom plan view, and
FIG. 9 is a sectioned side elevation view of the terminal. In this embodiment, a ventilation
terminal discharges air from a ventilation duct into a space with no change of direction
through the terminal. The configuration of this embodiment of the invention allows
the terminal to be mounted flush with a surface, such as a ceiling.
FIGS. 7 through
9 show ventilation terminal
10', the major components of which are inlet duct
13', terminal casing
14', inner wall member
16' and lobed array
22'.
[0027] Air from an upstream air supply duct (not shown) enters inlet duct
13' of terminal
10' through air inlet
11'. Lobed array
22' joins with the downstream end of inlet duct
13', therefore all of the air entering terminal
10' through air inlet
11' (primary air) must flow through primary flow passage
31', which is surrounded and defined by lobed array
22', before exiting terminal
10' through air outlet
12'. Air from the space served by terminal
10' (recirculating air) can enter the terminal through recirculating air inlet
33', which is an annular opening surrounding air outlet
12'. To exit through air outlet
12', air entering terminal
10' through recirculating air inlet
33' must pass through recirculating flow passage
34' and ejector flow passage
32'. Recirculating flow passage
34' is an annular space formed between the inner wall of terminal casing
14' and the outer wall of inner wall member
16'. Ejector flow passage
32' is an annular space formed by and between the inner wall of inner wall member
16' and lobed array
22'.
[0028] Lobed array
22' has a plurality of lobes
23' aligned longitudinally along the array. Lobes
23' penetrate alternately into both primary flow passage
31' and ejector flow passage
32' so that a lobe in one of the passages is a trough in the other. The height of lobes
23' increases gradually in an upstream to a downstream direction along the array. When
viewed from downstream (
FIG. 7), lobes
23' have a wave-like appearance. Taken together, lobed array
22', primary flow passage
31' and ejector flow passage
32' form a mixer ejector.
[0029] FIG. 10 shows schematically the operation of terminal
10'. Primary air enters terminal
10' through air inlet
11'. The primary air passes through terminal
10', passing through the lobes and troughs of lobed array
22' in primary flow passage
31'. Ejector mixing interaction between the air flow in primary flow passage
31' and the air in ejector flow passage
32' causes a flow of air to and through passage
32' from secondary air inlet
33', through recirculating air passage
34 and then to air outlet
12', causing air from the space served by terminal
10' to be drawn into the terminal and mixed with the primary air stream from the ventilation
supply duct. If desired, turning vanes or deflectors may be fitted at air outlet
12' to provide wider diffusion of the discharge of the terminal. The lower velocities
at the outlet would result in lower noise from such turning vanes, compared to conventional
vaned terminals.