U.S. patent number 3,734,653 [Application Number 05/173,895] was granted by the patent office on 1973-05-22 for screw compressor.
This patent grant is currently assigned to Gardner-Denver. Invention is credited to Soren E. H. Edstrom, John E. Seckman.
United States Patent |
3,734,653 |
Edstrom , et al. |
May 22, 1973 |
SCREW COMPRESSOR
Abstract
A liquid injected screw compressor having an intermediate
housing member which supports a detachable screw rotor housing
portion, a thrust bearing housing, and a pressure fluid control
actuator for a sliding capacity control valve. The intermediate
housing member also includes a cavity for distributing lubricating
and cooling oil to the compressor. The screw compressor includes a
substantially cylindrical casing fabricated of steel plate which is
bolted to the intermediate housing member and encloses the screw
rotor housing portion to serve as a pressure vessel for compressor
inlet gas and for gas vented by the capacity control valve. A
separate casing portion is bolted to the intermediate housing
member and encloses the thrust bearing housing and the pressure
fluid control actuator. The compressor is adapted to be mounted on
a base or frame by means of legs attached to the cylindrical
casing.
Inventors: |
Edstrom; Soren E. H. (Quincy,
IL), Seckman; John E. (Quincy, IL) |
Assignee: |
Gardner-Denver (Quincy,
IL)
|
Family
ID: |
22633966 |
Appl.
No.: |
05/173,895 |
Filed: |
August 23, 1971 |
Current U.S.
Class: |
418/88; 418/97;
418/201.2 |
Current CPC
Class: |
F04C
29/02 (20130101); F04C 28/24 (20130101); F04C
29/0007 (20130101); F04C 18/16 (20130101) |
Current International
Class: |
F04C
18/16 (20060101); F04C 29/02 (20060101); F04C
29/00 (20060101); F01c 001/16 (); F01c 021/04 ();
F04c 017/12 () |
Field of
Search: |
;418/87,88,97-99,197,201-203 |
References Cited
[Referenced By]
U.S. Patent Documents
Foreign Patent Documents
|
|
|
|
|
|
|
1,804,884 |
|
Sep 1970 |
|
DT |
|
1,628,385 |
|
Jan 1970 |
|
DT |
|
Primary Examiner: Croyle; Carlton R.
Assistant Examiner: Vrablik; John J.
Claims
What is claimed is:
1. In a screw compressor:
a rotor housing having two parallel intersecting bores forming a
working chamber;
an inlet port and a discharge port opening into said working
chamber;
a high pressure end wall at one end of said working chamber and a
low pressure end wall at the opposite end of said working
chamber;
interengaged male and female screw rotors located in said bores and
operable to entrap and compress gas admitted to said working
chamber through said inlet port, one of said rotors including a
shaft extension for connecting said one rotor to compressor driving
means;
valve means characterized by a movable wall portion of said working
chamber and operable to vent gas from said working chamber;
and,
a housing portion comprising an intermediate housing having a first
transverse face thereon, said first transverse face forming said
high pressure end wall of said working chamber, and said rotor
housing is removably fastened to said intermediate housing on said
first transverse face,
low pressure casing means including a gas inlet opening and means
defining an opening through which said shaft extension projects to
the exterior of said compressor, said compressor including sealing
means surrounding said shaft extension and sealingly engaged with
said means defining said opening, said low pressure casing means
including means for supporting said compressor on a frame, said low
pressure casing means substantially enclosing said rotor housing
and being removably fastened to said intermediate housing and in
sealing engagement to said first transverse face to form an
interior area between said rotor housing and said low pressure
casing means, said interior area defining a flow chamber in
communication with said inlet port and said valve means, and said
low pressure casing means comprises a member separable from said
intermediate housing whereby said compressor may be removed from
said low pressure casing means without moving said low pressure
casing means with respect to said frame.
2. The invention set forth in claim 1 wherein:
said low pressure casing means is fabricated of metal plate.
3. The invention set forth in claim 1 wherein:
said housing portion includes bearing means for rotatably
supporting the high pressure ends of said rotors.
4. The invention set forth in claim 1 wherein:
said intermediate housing includes a second transverse face spaced
from said first transverse face and a passageway opening through
said first and second transverse faces and being in communication
with said discharge port, said compressor includes housing means
including a chamber for a pressure fluid actuator, said actuator
being operable to move said valve means to vent gas from said
working chamber, said housing means being removably fastened to
said intermediate housing on said second transverse face, and said
compressor includes high pressure casing means including a
discharge opening, said high pressure casing means being adapted to
be removably fastened to said second transverse face in sealing
engagement therewith and substantially enclosing said housing means
and defining a discharge flow chamber in communication with said
passageway in said intermediate housing for receiving compressed
gas from said working chamber.
5. In a screw compressor:
a rotor housing having two parallel intersecting bores forming a
working chamber;
an inlet port and a discharge port opening into said working
chamber;
a high pressure end wall at one end of said working chamber and a
low pressure end wall at the opposite end of said working
chamber;
interengaged male and female screw rotors located in said bores and
operable to entrap and compress gas admitted to said working
chamber through said inlet port;
a housing portion including bearing means for supporting the high
pressure ends of said rotors, said housing portion having a first
transverse face and a second transverse face spaced from said first
transverse face;
low pressure casing means removably fastened to said first
transverse face and substantially enclosing said rotor housing and
forming an interior area between said low pressure casing means and
said rotor housing defining a gas inlet flow chamber;
high pressure casing means removably fastened to said second
transverse face, said high pressure casing means forming with said
second transverse face a compressor gas discharge flow chamber;
and,
means for conducting liquid to said working chamber including a
cavity in said housing portion, conduit means for conducting liquid
from an external source to said cavity, and conduit means for
conducting liquid from said cavity to said working chamber.
6. The invention set forth in claim 5 wherein:
said compressor includes liquid pump means supported by said
housing portion and disposed within said discharge flow chamber
formed by said second transverse face and said high pressure casing
means.
7. The invention set forth in claim 5 wherein:
said conduit means for conducting liquid from said cavity are
disposed within the chambers defined by said casing means.
8. The invention set forth in claim 5 wherein:
said housing portion includes flow control means disposed in flow
communication with said cavity and operable to limit the flow of
liquid from said cavity to said working chamber.
9. The invention set forth in claim 8 wherein:
said flow control means comprises a plug having an orifice therein,
a holder for said plug, said plug and said holder being removably
insertable in said housing portion.
10. The invention set forth in claim 9 wherein:
said cavity includes a portion opening to the exterior of said
compressor and said holder is removably insertable in said cavity
portion from the exterior of said compressor.
Description
BACKGROUND OF THE INVENTION
Liquid injected gas compressors of the helical screw rotor type are
well known and are used in many applications including
refrigeration and other gas process systems. In particular, in
applications such as vapor-compression refrigeration systems, it is
desirable to have high efficiency capacity control devices whereby
the compressor may be operated economically at part load
conditions. To this end there has been developed what is known in
the art as the axial slide valve capacity control. Such a control
device is generally characterized by an axially movable portion of
the screw rotor housing wall which in effect shortens the length of
the intermeshing screw rotors and thereby reduces their swept
volume in compression. Examples of axial slide valve controlled
screw compressors are disclosed in U.S. Pat. Nos. 3,314,597 and
3,432,089 to L.B. Schibbye.
Generally, axial slide valve controlled screw compressors are also
designed to operate with compressor inlet pressures substantially
greater than atmospheric pressure. Accordingly, in prior art screw
compressors the compressor housing containing the screw rotors and
the axial slide valve has been formed as a substantially thick
walled metal casting. Cast prior art compressor housings have not
only been of heavy section thickness to withstand high gas
pressures but the gas return passages communicating gas vented from
the slide valve back to the compressor inlet have resulted in a
rather complicated and difficult to clean casting.
A related problem in the art of liquid injected screw compressors
concerns the leakage of gas and the injection liquid from the
numerous piping connections normally required, and from the flanged
joints between compressor housing pieces. Leakage of gas under
pressure to the exterior of the compressor is particularly unwanted
in a closed system and when the gas being compressed is toxic or
flammable. Of course, leakage of the injection liquid is also
unwanted. Therefore, it is desirable to minimize the number of
compressor housing joints and to make such joints easily sealable.
Furthermore, the numerous external piping connections and conduits
found in prior art compressors precludes the effective application
of noise suppression coatings or wrappings on the compressor
housing.
In certain prior art screw compressor designs the liquid injection
system is substantially contained within the screw rotor housing
portion wherein a cavity is formed in the housing proper adjacent
to the rotor bores. All liquid injection and lubricant flow
passages are internally formed to be in communication with said
cavity. Such an arrangement is disclosed in U.S. Pat. No. 3,178,104
to R.F. Williams, et al. However, the benefits of this type of
liquid distribution arrangement have not heretofore been enjoyed in
compressors having the afore-mentioned sliding valve capacity
control device. Moreover, in prior art screw compressors used for
refrigeration and other high pressure gas service the problem of
gas and liquid leakage has in some cases been dealt with by placing
the entire compressor in a hermetically sealed enclosure which
greatly increases the bulk of the machine and makes servicing
difficult and time consuming.
SUMMARY OF THE INVENTION
The present invention is directed to an improved housing
construction for liquid injected helical screw gas compressors
which provides for a minimum number of housing joints required to
be hermetically sealed and which provides for a liquid distribution
system which is substantially contained within the compressor
housing.
The present invention also provides for a housing construction for
a helical screw gas compressor of the sliding valve capacity
control type wherein an inlet casing portion is separately formed
as a fabricated metal member for enclosing the screw rotor housing
to form a chamber for compressor inlet gas and for gas vented by
the capacity control valve. The fabricated casing portion is also
formed to provide for supporting the compressor unit on a frame and
the compressor may be bodily detached from the fabricated casing
portion without disturbing the alignment thereof with respect to
the compressor drive motor.
The present invention further provides a housing construction for a
liquid injected helical screw compressor in which an intermediate
housing member comprises a support for the basic compressor proper
and which is readily detachable from the fabricated casing portion.
The intermediate housing member also includes a liquid distribution
cavity or manifold which provides for a minimum number of liquid
conduit connections to be located on the exterior of the
compressor. The arrangement of a liquid distribution cavity in an
intermediate housing member together with hermetically sealable
casing portions mounted thereon provides for substantially all
liquid conduits to be located within enclosed areas which are
normally exposed to the compressor gas-liquid mixture. The
compressor housing construction of the present invention also
provides a structure which is aesthetically pleasing as well as
being easily covered with externally applied sound absorbing and
insulating blankets or coatings.
BRIEF DESCRIPTION OF THE DRAWINGS
FIG. 1 is an exterior longitudinal elevation of a helical screw
compressor in accordance with the present invention.
FIG. 2 is an exterior transverse elevation of the compressor of
FIG. 1.
FIG. 3 is a longitudinal section of a helical screw compressor
according to the present invention taken substantially along the
line 3--3 of FIG. 4.
FIG. 4 is a transverse section taken along the line 4--4 of FIG.
3.
FIG. 5 is a section taken along the line 5--5 of FIG. 4.
FIG. 6 is a perspective view showing the compressor disassembled
from the exterior casing portions.
FIG. 7 is a schematic of the liquid injection and lubrication
system of the compressor of the present invention.
FIG. 8 is a fragmentary view taken along the line 8--8 of FIG. 3
with the high pressure casing removed.
FIG. 9 is a section view taken along the line 9--9 of FIG. 3 with
the low pressure casing removed.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
Referring to FIGS. 1-4 and 6, a liquid injected screw compressor
according to the present invention is illustrated and generally
designated by the numeral 10. The compressor 10 is of a type
generally well known in which a pair of cooperating rotors, a male
rotor 12, and a female rotor 14, are rotatably housed in a rotor
housing 16 having parallel intersecting bores 18 and 20 surrounding
in close fitting relationship the respective rotors 12 and 14. The
male rotor 12 has four helical lobes 22 and intervening grooves 24
and the female rotor 14 has six helical lobes 26 and intervening
grooves 28. Various rotor lobe profiles and lobe wrap angles as
well as combinations of numbers of lobes on the respective rotors
are known and used in the art of screw compressors. However, for
high pressure ratio liquid injected screw compressors a male-female
lobe combination of four and six respectively with respective wrap
angles of 300.degree. and 200 degrees have been found desirable.
The rotors 12 and 14 are drivably interengaged to operate without
synchronizing gears.
The rotor housing 16 is removably bolted to an intermediate housing
30 having a first transverse face 32 which forms the high pressure
end wall of the compression or working chamber comprising the bores
18 and 20. The opposite end of the rotor housing 16 is partially
closed by a bearing housing 34 removably bolted thereto and
including a low pressure or inlet port 36 which opens through the
end wall 37 into the working chamber. The inlet port 36 is
primarily axial in accordance with known design practice for
helical screw compressors. The rotor housing 16 also includes an
integral wall portion 38 forming a bore 40 for an axially slidable
valve member 42 which comprises a portion of the wall defining the
working chamber formed by the intersecting bores 18 and 20. The
valve member 42 is similar to the axially slidable valve disclosed
in U.S. Pat. No. 3,314,597. The valve member 42 is axially slidable
in the bore 40 from the closed position shown, viewing FIG. 3, to a
position to the right whereby an opening is formed between the edge
44 and the valve member through which gas entrapped in the rotor
grooves 24 and 28 may be vented from the compressor working
chamber. The axially slidable valve member 42 thereby operates as a
control over the swept volume or compressed gas throughput of the
compressor 10. The valve member 42 is guided by a cylindrical pin
46 fitted in cooperating grooves 48 and 50 in the valve member 42
and in the wall portion 38, respectively.
As may be seen in FIG. 3 the male rotor 12 is rotatably supported
in a radial sleeve type bearing 52 on the low pressure end of the
rotor and in a similar bearing 54 on the high pressure end of the
rotor. The bearings 52 and 54 are respectively located in the
bearing housing 34 and the intermediate housing 30. Axial forces
acting on the rotor 12 are partially taken by a pair of angular
contact ball bearings 56. The bearings 56 are suitably housed in a
bearing housing 58 which is removably bolted to the intermediate
housing 30 on a second transverse face 59 spaced from and parallel
to the face 32. The bearing housing 58 includes a cylindrical
chamber 60 in which is located a thrust piston 62 which is attached
to the high pressure end portion 63 of the male rotor 12. Pressure
fluid such as the compressor injection liquid is conducted to the
chamber 60 to act on the piston 62 to offset the thrust forces due
to the high pressure gas acting on the end face 64 of the rotor 12.
The opposite end of the male rotor 12 includes an integral shaft
portion 66 to which a prime mover may be connected by means of a
coupling 68 as shown in FIG. 1. The female rotor 14 is similarly
supported by sleeve bearings and rolling element thrust bearings,
not shown. The female rotor also includes a thrust piston formed by
the end of the rotor shaft extension, not shown, located in the
bearing housing 34. The thrust piston on the female rotor 14 also
acts in a known way to oppose the axial thrust forces acting on the
female rotor.
The bearing housing 58 also includes a cylindrical bore forming a
chamber 70 for a pressure liquid operated actuator. A piston 72
slidable in the chamber 70 comprises an integral portion of the
sliding valve member 42 and is connected to the valve member by
spaced apart longitudinal webs 74, one shown in FIG. 3. The webs 74
extend through an open area 76 in the intermediate housing 30 which
forms a passageway for a high pressure gas-liquid mixture being
discharged from the compressor working chamber through a discharge
port 78 formed in the face 32 of the intermediate housing 30 and by
the edge 80 of the sliding valve member 42. The piston 72 includes
a member 82 removably attached thereto comprising a nut threadedly
engaged with a rotatable screw 84. The screw 84 is rotatably
journaled in a bearing 86 located in a cover member 88 for the
chamber 70. The screw 84 is operable to be connected to suitable
mechanism, not shown, for indicating the position of the piston 72
and sliding valve member 42. The piston 72 is operable to move the
sliding valve member to the left, as shown in FIG. 3, in response
to the admission of pressure fluid to the chamber 70.
The sliding valve member 42 is biased against the forces acting on
the piston 72 due to pressure fluid in the chamber 70 by a coil
spring 90 supported by a tubular guide 92 attached to the bearing
housing 34. The coil spring 90 operates to move the valve member 42
to the full open or minimum capacity position in the absence of
pressure fluid being applied to act on the piston 72. Moreover, the
axial projected area of the piston face 94 is greater than the
axial projected area of the face 96 of the valve member 42 so that
a bias force tending to open the valve to reduce compressor
throughput is created by the high pressure gas in the area 76. This
feature provides for assuring that the valve member 42 will move to
reduce the required work input to the compressor in the absence of
pressure fluid in the chamber 70 such as during compressor
startup.
A particularly advantageous feature of the compressor 10 in
accordance with the present invention is realized with the
construction wherein a substantially cylindrical low pressure
casing 98 is formed to be detachably bolted to the transverse face
32 of the intermediate housing 30 and enclosing the rotor housing
16 and the bearing housing 34. The casing 98 includes a flanged
inlet opening 100 for compressor inlet gas. The interior area 102
between the rotor housing 16 and the casing 98 comprises an inlet
flow chamber to the compressor inlet port 36 and also for receiving
gas vented from the working chamber by the sliding capacity control
valve 42. The casing 98 is preferably formed of fabricated metal
such as steel in accordance with accepted pressure vessel design
practices and includes an annular flange 104 for fastening the
casing to the intermediate housing 30. The casing 98 includes a
sleeve 106 suitably welded to the casing and forming an opening
through which the male rotor shaft extension 66 projects. The
sleeve 106 sealingly engages the exterior of a rotary mechanical
seal assembly 108 for the male rotor shaft. The casing 98 also
includes a plurality of legs 110 for supporting the compressor on a
frame 112 as shown in FIGS. 1 and 2. Contrary to prior art screw
compressors of the axial slide valve capacity controlled type the
compressor 10 of the present invention comprises a rotor housing 16
which may be a metal casting of comparatively simple construction
and being relatively easy to manufacture. Thanks to the provision
of the fabricated casing 98 as a member separable from the rotor
housing 16, and which is lighter in weight and inherently less
susceptible to structural defects as compared to a casting, the
compressor 10 is less costly to manufacture and, furthermore,
enjoys ease of assembly and disassembly as will be explained
herein.
The screw compressor according to the present invention also
includes a high pressure casing 114 removably fastened to the
transverse face 59 of the intermediate housing 30. The casing 114
is characterized by a hollow interior 116 forming a discharge flow
chamber which is in communication with the area 76 in the
intermediate housing 30 through openings 118 in the transverse face
59, FIG. 8. The casing 114 also includes a flanged opening 120 for
connecting a suitable conduit to the compressor 10 to conduct high
pressure gas and liquid from the compressor. As may be noted in
FIG. 3 the casing 114 encloses the bearing housing 58 and includes
a boss 122 having a cylindrical opening for sealingly receiving a
cylindrical portion 124 of the cover member 88.
The casings 98 and 114 are easily disassembled from the
intermediate housing 30 by removing the screws 126 around the
flanges 104 and 128 respectively. The cylindrical flanged joints
between the casings 98 and 114 and the intermediate housing 30 are
also easily sealed by conventional O-rings 130 located in suitable
grooves in the intermediate housing. As best illustrated in FIG. 6
the compressor 10 may be disassembled, without disturbing the
alignment of the casing 98 with respect to a prime mover, by
unbolting the flanged joint between the intermediate housing 30 and
the casing 98 whereby the entire compressor with the exception of
the casing 98 may be moved to a suitable location for servicing and
further disassembly. Moreover, if access to the bearing housing 58
or any of the components located in the interior of the casing 114
is desired the casing 114 may be easily removed from the
intermediate housing. Alignment of the casings 98 and 114 with
respect to the compressor assembly comprising the intermediate
housing and the housing members fastened thereto may be achieved by
conventional means such as dowel pins 132, one shown in FIG. 6.
As previously mentioned the compressor 10 is of a well known type
in which liquid is injected into the working chamber formed by the
bores 18 and 20 to be mixed with the gas being compressed for
absorbing some of the heat of compression and for sealing the
clearances between the cooperating rotors 12 and 14. The liquid is
usually a suitable oil which also serves as a lubricant for the
interengaged rotors and the rotor bearings. The liquid used for
lubrication as well as what is directly injected into the
compressor working chamber is discharged with the high pressure
gas, separated from the gas, cooled and recirculated through the
compressor in a known manner.
In accordance with the present invention there is provided a
housing construction which provides for an improved liquid
distribution system which is substantially enclosed within the
casings 98 and 114, and thereby minimizes leakage of liquid to the
exterior of the compressor. In the compressor 10 the intermediate
housing 30 includes a plurality of passages for conducting liquid
to various locations in the compressor. The intermediate housing 30
also includes a cavity or manifold 134 from which pressure liquid
is distributed. Referring in particular to FIGS. 3 through 7 liquid
is introduced into the compressor proper through a conduit 136 and
a passageway 138 in the intermediate housing 30 to a suitable pump
140 driven by an extension, not shown, of the female rotor. The
pump 140 provides for increasing the pressure of the liquid to a
value sufficient to provide adequate force on the thrust piston 62
as well as liquid flow to all desired locations within the
compressor. A discharge conduit 142 from the pump 140 is connected
to a passage 144 in the intermediate housing which is in
communication with a filter 146 fastened to the intermediate
housing. Liquid from the filter 146 flows into the cavity 134 in
the intermediate housing.
The cavity 134 serves as a manifold for distributing pressure
liquid to the compressor bearings and seals, the thrust pistons,
the working chamber formed by the intersecting bores 18 and 20, and
the chamber 70 of the actuator for the capacity control valve 42.
Pressure liquid is supplied to the chamber 70 from the cavity 134
through conduits 148, 150, passage 152 and conduit 154. A suitable
valve 156 is interposed in the conduit 148 to control the flow of
pressure liquid to the chamber 70 of the capacity control valve
actuator. Pressure liquid is vented from the chamber 70 by
operation of valve 158 interposed in the conduit 160. The conduit
160 is in communication with conduit 150 and a passage 162 in the
intermediate housing which opens into the interior 102 of the
casing 98. A substantial portion of the liquid discharged into the
interior 102 is eventually entrained with the inlet gas flowing to
the compressor working chamber. The cavity 134 also is in
communication with a pressure relief valve 163 shown in FIG. 5 and
schematically shown in FIG. 7. The pressure relief valve 164 is
operable to limit the liquid pressure in the cavity 134 and
operates to vent liquid into the interior 116 of the casing 114.
The relief valve 164 is of a type which operates basically on the
pressure differential existing between the interior 116 and the
cavity 134.
The cavity 134 includes a portion 166, FIG. 5, interconnected by a
passage 168 to the cavity and including a passage 170 leading to
the bearings 54 located in the intermediate housing. A conduit 172
also leads from the cavity portion 166 to the thrust piston chamber
60 for supplying pressure liquid to act on the thrust piston 62.
Liquid leaking past the periphery of the thrust piston to a chamber
174 formed by the cover portion 175, FIG. 3, is conducted away from
said chamber by a conduit 176 which is connected, via a suitable
passage in the intermediate housing, to a conduit 178 leading to
the bore 20. A conduit 180 also connected to the cavity portion 166
supplies liquid to the bearings 52 in the bearing housing 34 and to
a thrust piston on the female rotor 14 which as previously
mentioned is also located in the bearing housing 34. Liquid is also
supplied to the shaft seal assembly 108 by way of conduit 182 and
is drained from the seal to the conduit 178 through a connecting
conduit 184.
Liquid draining from the compressor bearings and from the thrust
pistons and the seal 108 flows into the working chamber comprising
the intersecting bores 18 and 20. The primary source of liquid
injected into the working chamber is, however, from a conduit 186
in communication with the cavity portion 166 and connected to a
passageway 188 located in the integral wall portion 38 of the rotor
housing 16. The passageway 188 is in communication with an annular
area 190 and intersecting passages 192, 194, and 196 in the
locating pin 46. As shown in FIG. 4 the passage 196 in the pin 46
opens into an annular area 198 which is in communication with
peripheral grooves 200 which open into the bores 18 and 20. The
grooves 200 conduct injection liquid into the working chamber of
the compressor in a region which is normally subject to high
pressure gas under compression. The location of the grooves 200 in
the bore 40 also serves to provide liquid for lubricating the
bearing surface formed by the bore 40 to facilitate easy movement
of the axial sliding valve member 42.
The compressor 10 is adapted to be used in various
vapor-compression refrigeration systems utilizing different types
of refrigerants. The ratio of injection liquid mass flow to
refrigerant gas mass flow for optimum compressor performance has
been determined to be dependent on the type of refrigerant used in
the system. The flow rate of injection liquid to the grooves 200 is
controlled by means comprising an orifice plug holder 202 which, as
shown in FIG. 5, is removably insertable from the exterior of the
intermediate housing 30 into the cavity portion 166. The holder 202
includes a removable plug 204 having an orifice 206 which opens
into a passageway 208 in the holder from the cavity portion 166.
The passage 208 in the holder opens into the annular area 210
formed by the holder and the cavity portion 166. The area 210 is in
communication with the conduit 186. As may be appreciated from the
foregoing the arrangement of the holder 202 in the intermediate
housing 30 provides for interchanging the plug 204 with similar
plugs having different orifice sizes without disassembly of the
compressor.
Referring to FIG. 9, a second set of grooves 212 are also formed in
the wall portion 38 and open into the intersecting bores 18 and 20.
In FIG. 9 an alternate embodiment of a cylindrical locating pin 214
is shown in which is formed an annular recess 216 in communication
with the grooves 212 and the passage 188. The grooves 212 and the
pin 214 are used to provide an alternate location for liquid
injection into the compressor working chamber for use with
alternate embodiments of the axial sliding valve member 42. Such
alternate embodiments of the sliding capacity control valve are
used for changing the so-called built-in volume ratio of the
compressor.
As may be appreciated from the foregoing description of the liquid
injection and lubrication system the provision of a distribution
cavity or manifold in the intermediate housing 30 and the location
of substantially all conduits within the casings 98 and 114
eliminates, to a large extent, leakage of the injection liquid to
the exterior of the compressor 10. Moreover, the joints formed
between the intermediate housing, the rotor housing 16 and the
bearing housings 34 and 58 are not required to be completely fluid
tight. Gas and liquid leakage between the connection flanges of the
aforementioned housing, small amounts of which can be tolerated
from a compressor performance standpoint, merely flows into the
chambers formed by the interiors of the casings 98 and 114.
* * * * *