US3131855A - Art of conserving lubricant in gas compressors - Google Patents

Art of conserving lubricant in gas compressors Download PDF

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US3131855A
US3131855A US162685A US16268561A US3131855A US 3131855 A US3131855 A US 3131855A US 162685 A US162685 A US 162685A US 16268561 A US16268561 A US 16268561A US 3131855 A US3131855 A US 3131855A
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pressure stage
crankcase
stage
high pressure
low pressure
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US162685A
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Erich J Kocher
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Copeland Industrial LP
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Vilter Manufacturing LLC
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B31/00Compressor arrangements
    • F25B31/002Lubrication
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B1/00Compression machines, plants or systems with non-reversible cycle
    • F25B1/10Compression machines, plants or systems with non-reversible cycle with multi-stage compression
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2400/00General features or devices for refrigeration machines, plants or systems, combined heating and refrigeration systems or heat-pump systems, i.e. not limited to a particular subgroup of F25B
    • F25B2400/13Economisers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25BREFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B2400/00General features or devices for refrigeration machines, plants or systems, combined heating and refrigeration systems or heat-pump systems, i.e. not limited to a particular subgroup of F25B
    • F25B2400/23Separators

Definitions

  • the principal object of this invention is to prevent excessive escape of oil from the lubricating system of a compound gas compressor especially of the two-stage reciprocating piston type, and to thereby maintain proper lubrication of the compressor.
  • Another important object of the invention is to provide a system whereby simple but dependable apparatus may be utilized to minimize the loss of lubricant in a twostage gas compressor of the reciprocating piston type wherein both cylinders are exposed to a common crankcase.
  • FIG. 1 is a diagram of a refrigeration system adapted to exploit the present invention, and embodying two-stage compression wherein the compressors are shown separate y;
  • FIG. 2 is an enlarged central vertical section through a typical two-stage reciprocating piston gas compressor such as shown diagrammatically in PEG. 1.
  • the refrigerating system shown therein comprises in general a two-stage system having low and high stage compressors 5, 6, respectively; an intercooler 7 interposed between the compression stages 5, 6; a condenser 8 connected to the high pressure stage 6; a receiver 9 communicating with the condenser 8; an evaporator 19 adapted to receive liquid refrigerant from the receiver 9 past an expansion valve 11 and to deliver spent refrigerant gas through a passage 12 into the suction of the low pressure stage 5; and a conduit 13 connecting the crankcase of the high pressure stage 6 with the passage 12 and having a bleeder valve 14 therein.
  • FIG. 1 discloses the use of an intercooler 7 between compression stages, this is not essential, but when used, the lower portion of the intercooler is connected with the discharge of the low pressure stage 5 by a conduit 16, a medial portion communicates with the discharge line 17 or" the receiver 9 through a conduit 13 and past a float valve 19 operable to control the quantity of liquid refrigerant admitted to the intercooler, and the upper portion of the latter above the liquid level is connected with the suction of the high pressure stage 6 by another conduit 2%.
  • the discharge or" the high pressure stage communicates with the condenser 3 by a conduit 21 and the latter is connected with the receiver 9 by a connection 22 thus completing the refrigeration system.
  • the intercooler is omitted, and the compressor comprises a pair of identical low pressure stages 5 cooperating with the same high pressure stage 6 all mounted in the same casing 23 having a common crankcase 24 containing oil for lubricating the bearings and moving parts of all stages.
  • the two low pressure pistons 25 are reciprocable within fixed cylinders 26, and the single high pressure piston 27 is simultaneously reciprocable within a fixed cylinder 28 by means of the same crankshaft 29 which is rotatable within the crankcase 24 and is adapted to splash lubricating oil from Within the latter into all of the cylinders 26, 28.
  • the compressor may embody several of such stage sets located laterally adjacent to each other and operable by the same crankshaft 29, depending upon the capacity required, and this crankshaft may be rotated from any suitable power source such as an electric motor. 7
  • the discharge conduits 16 of the two lower pressure stage sections both communicate directly with the high pressure stage intake conduits 2i and are connected with the single crankcase 24 by one or more restricted ports 31 while the suction side of each low pressure stage 5 is likewise connected with this crankcase by ports 32 which correspond to the conduit 13 of FIG. 1 but do not embody a bleeder valve 14 since the ports 32 may be made sufficiently restricted so as to function as blecders and maintain a lower pressure in the crankcase than in the high pressure chamber 6 in order that oil in the cylinder 23 is drawn down into the crankcase 24.
  • Each stage of the compressor is provided with an annular inlet valve 33 and with an outlet valve 1% both located at the same end of its cylinder 26, 28, such valves being of well-known construction and therefore being shown only in the high pressure stage 6 of FIG. 2.
  • the crankshaft 29 will be revolving at relatively high speed to reciprocate the pistons 25, 27 and to splash oil from within the crankcase 3 24 into the cylinders 26, 28.
  • the two sections of the low pressure stage 5 will withdraw refrigerant gases from the evaporator it) through the passage 12 and will initially an intercooler 7 if used.
  • the high pressure stage 6 will then further compress these gases and discharge the same through the conduit 21 into the condenser 8 wherein the high pressure refrigerant is liquified and delivered through the connection 22 into the receiver 9.
  • the evaporator 10 will thereafter withdraw high pressure liquid refrigerant as required from the receiver through the pipe line 17 and past the expansion valve 11, and as this liquid refrigerant is converted into gas in the evaporator it is withdrawn through the passage 12 to complete the cycle.
  • this entrained oil will enter the high compressor pressure stage 6 in considerable quantity. Besides the fact that such entry 'of incompressible liquid into the high pressure stage 5 may damage the piston 27, the escaping oil if not removed from the high pressure stage discharge will be carried by the refrigerant into the condenser 8, a receiver 9, and evaporator 19, thus reducing the efliciency of the entire system and alsorresulting in loss of considerable oil.
  • the present invention therefore provides a method of efiectively preventing escape of excessive quantities of lubricating oil with the finally compressed refrigerant gas,.
  • the system for minimizing lubricating. oil loss in a multi-stage reciprocating piston gas compressor having at least one high pressure stage and one low pressure stage provided with a crankcase which comprises, conduit means interconnecting the discharge of said low pressure stage with the high pressure stage crankcase and conduit means also interconnecting said crankcase with the suction zone of said low pressure stage of the compressor to induce the oil to flow from said low pressure stage dis charge into the crankcase.
  • wvhereby lubricating oil may escape from the discharge of saidloW pressure stage into said crankcase via said first conduit means.
  • a' crankcase In a refrigerating system having at least one low pressure stage and one high pressure stage cylinder each containing a reciprocating piston for circulating refrigerant within the system, a' crankcase, conduit means connecting the outlet end of the low pressure stage cylinder with the crankcase, and other conduit means connecting said crankcase with the suction inlet of the low pressure stage.

Description

y 5, 1954 E. J. KOCHER 3,131,855
ART OF CONSERVING LUBRICANT IN GAS COMPRESSORS Filed Dec. 28, 1961 I 5 29 :31 4 Q Y 2.2
n In 9 /Z-- INVENTOR. E .1 K 04-1152 AT a/ewzv:
United States Patent Office 3,131,855. Patented May 5, 1964 3,131,855 ART ()1 CONSERVENG LUBRICANT 1N GAS COMERESSQRS Erich 3. Kosher, Milwaukee, Wis, assignor to Vilter Manufacturing Corporation, Milwaukee, WE, a corporation of Wisconsin Filed Dec. 28, E61, Ser. No. 162,685 5 Claims. (Cl. 23il206) The present invention relates in general to improvements in the art of conserving lubricant in gas compressors, and it relates more specifically to an improved method or system for minimizing the loss of lubricating oil in multi-stage refrigerant compressors.
The principal object of this invention is to prevent excessive escape of oil from the lubricating system of a compound gas compressor especially of the two-stage reciprocating piston type, and to thereby maintain proper lubrication of the compressor.
It has heretofore been customary in single-acting refrigerant compressors of the reciprocating piston type to maintain a body of lubricating oil for the crankshaft bearings and the piston in the bottom of the crankcase and to drain oil which escapes with the compressed gases back into the oil supply within the crankcase in various ways. Excessive escape of lubricant with the compressed gases in a single-stage compressor may thus be avoided, but considerable difliculty has heretofore been encountered when attempting to avoid such loss of oil in multi-stage compressors wherein both low and higher pressure cylin ders are in open communication with a common crankcase while the discharge chambers of the lower stages communicate with the intake chamber of a subsequent higher compression stage.
It is therefore an important object of the present invention to provide an improved method of effectively preventing loss of lubricant with the compressed gas finally delivered by a multi-stage compressor in order to insure proper lubrication of the working parts of such machines at all times.
Another important object of the invention is to provide a system whereby simple but dependable apparatus may be utilized to minimize the loss of lubricant in a twostage gas compressor of the reciprocating piston type wherein both cylinders are exposed to a common crankcase.
These and other more specific objects and advantages of the invention will be apparent from the following detailed description.
A clear conception of the several steps involved in the present improved method, and of the construction and functioning of a typical refrigeration system having a twostage compressor for effecting operation of the system, may be had by referring to the drawing accompanying and forming a part of this specification wherein like reference characters designate the same or similar parts in the several views.
FIG. 1 is a diagram of a refrigeration system adapted to exploit the present invention, and embodying two-stage compression wherein the compressors are shown separate y; and
FIG. 2 is an enlarged central vertical section through a typical two-stage reciprocating piston gas compressor such as shown diagrammatically in PEG. 1.
While the invention has been shown and described herein as being advantageously applicable to a system embodying a compressor of the type specifically illustrated in FIG. 2, it is not intended to limit its application to a two-stage compressor embodying several low pressure stages cooperating with the same high pressure stage; and
it is also contemplated that specific descriptive terms employed herein be given the broadest possible interpretation consistent with the disclosure.
Referring to FIG. 1, the refrigerating system shown therein comprises in general a two-stage system having low and high stage compressors 5, 6, respectively; an intercooler 7 interposed between the compression stages 5, 6; a condenser 8 connected to the high pressure stage 6; a receiver 9 communicating with the condenser 8; an evaporator 19 adapted to receive liquid refrigerant from the receiver 9 past an expansion valve 11 and to deliver spent refrigerant gas through a passage 12 into the suction of the low pressure stage 5; and a conduit 13 connecting the crankcase of the high pressure stage 6 with the passage 12 and having a bleeder valve 14 therein.
While the diagram of FIG. 1 discloses the use of an intercooler 7 between compression stages, this is not essential, but when used, the lower portion of the intercooler is connected with the discharge of the low pressure stage 5 by a conduit 16, a medial portion communicates with the discharge line 17 or" the receiver 9 through a conduit 13 and past a float valve 19 operable to control the quantity of liquid refrigerant admitted to the intercooler, and the upper portion of the latter above the liquid level is connected with the suction of the high pressure stage 6 by another conduit 2%. The discharge or" the high pressure stage communicates with the condenser 3 by a conduit 21 and the latter is connected with the receiver 9 by a connection 22 thus completing the refrigeration system.
As illustrated in FIG. 2, the intercooler is omitted, and the compressor comprises a pair of identical low pressure stages 5 cooperating with the same high pressure stage 6 all mounted in the same casing 23 having a common crankcase 24 containing oil for lubricating the bearings and moving parts of all stages. in this twostage compressor, the two low pressure pistons 25 are reciprocable within fixed cylinders 26, and the single high pressure piston 27 is simultaneously reciprocable within a fixed cylinder 28 by means of the same crankshaft 29 which is rotatable within the crankcase 24 and is adapted to splash lubricating oil from Within the latter into all of the cylinders 26, 28. While only one set of low and high pressure stages 5, 6 is illustrated, the compressor may embody several of such stage sets located laterally adjacent to each other and operable by the same crankshaft 29, depending upon the capacity required, and this crankshaft may be rotated from any suitable power source such as an electric motor. 7
In the compressor of FIG. 2, the discharge conduits 16 of the two lower pressure stage sections both communicate directly with the high pressure stage intake conduits 2i and are connected with the single crankcase 24 by one or more restricted ports 31 while the suction side of each low pressure stage 5 is likewise connected with this crankcase by ports 32 which correspond to the conduit 13 of FIG. 1 but do not embody a bleeder valve 14 since the ports 32 may be made sufficiently restricted so as to function as blecders and maintain a lower pressure in the crankcase than in the high pressure chamber 6 in order that oil in the cylinder 23 is drawn down into the crankcase 24. Each stage of the compressor is provided with an annular inlet valve 33 and with an outlet valve 1% both located at the same end of its cylinder 26, 28, such valves being of well-known construction and therefore being shown only in the high pressure stage 6 of FIG. 2.
When the refrigeration system and its compressor have been constructed and assembled as above described and properly adjusted, it functions as follows while exploiting the present improved method. The crankshaft 29 will be revolving at relatively high speed to reciprocate the pistons 25, 27 and to splash oil from within the crankcase 3 24 into the cylinders 26, 28. The two sections of the low pressure stage 5 will withdraw refrigerant gases from the evaporator it) through the passage 12 and will initially an intercooler 7 if used. The high pressure stage 6 will then further compress these gases and discharge the same through the conduit 21 into the condenser 8 wherein the high pressure refrigerant is liquified and delivered through the connection 22 into the receiver 9. The evaporator 10 will thereafter withdraw high pressure liquid refrigerant as required from the receiver through the pipe line 17 and past the expansion valve 11, and as this liquid refrigerant is converted into gas in the evaporator it is withdrawn through the passage 12 to complete the cycle.
While'the' system is operating in this manner, considerable lubricating oil is mixed with and carried by the refrigerant through sections of the low pressure stage 5, and if the pressures Within the crankcase 24' and in the high pressure stage suction conduit 29 are not equalized,
this entrained oil will enter the high compressor pressure stage 6 in considerable quantity. Besides the fact that such entry 'of incompressible liquid into the high pressure stage 5 may damage the piston 27, the escaping oil if not removed from the high pressure stage discharge will be carried by the refrigerant into the condenser 8, a receiver 9, and evaporator 19, thus reducing the efliciency of the entire system and alsorresulting in loss of considerable oil. But by connecting'the low pressure discharge conduits 16 with the high pressure crankcase 24- as with ports 31 and by also connecting the crankcase 24- With the lower pressure stage suction zones as by ports 32, the pressuresin the crankcase andlow pressure suction maybe substantially equalized thus permitting the oil from within the suction chamber of the high pressure stage 6 to drain by gravity into the crankcase 24 so that this oil cannot enter the compression chamber of the high pressure stage. i V
The present invention therefore provides a method of efiectively preventing escape of excessive quantities of lubricating oil with the finally compressed refrigerant gas,.
and which can be carried on automatically with the aid of simple equipment or apparatus. The removal and return of the entrained oil to the crankcase 24 also insures proper lubrication of all moving parts of the compressor and insures most eificient functioningof the entire refrigeration system while in operation. The improved method is obviously capable of being exploited with various types of multi-stage compressors regardless of whether, all stages are housed within a common casing or whether one or more low pressure stages precede the final high pressure stage.
Various modes of carrying out the invention are contemplated as being within the scope of the following claims particularly pointing out and distinctly claiming the subject matter which is regarded as the invention.
' I claim:
1. The system for minimizing lubricating. oil loss in a multi-stage reciprocating piston gas compressor having at least one high pressure stage and one low pressure stage provided with a crankcase, which comprises, conduit means interconnecting the discharge of said low pressure stage with the high pressure stage crankcase and conduit means also interconnecting said crankcase with the suction zone of said low pressure stage of the compressor to induce the oil to flow from said low pressure stage dis charge into the crankcase.
2. In a refrigerating system having at least one low' pressure stage and one high pressure stage reciprocating piston for circulatingrefrigerant within the system, a 7
- ing the discharge of the low pressure stage with the common crankcase, and other conduit means connecting said crankcase with the suction inlet of the low pressure stage,
wvhereby lubricating oil may escape from the discharge of saidloW pressure stage into said crankcase via said first conduit means.
4. In a refrigerating system having at least one low pressure stage and one high pressure stage cylinder each containing a reciprocating piston for circulating refrigerant within the system, a' crankcase, conduit means connecting the outlet end of the low pressure stage cylinder with the crankcase, and other conduit means connecting said crankcase with the suction inlet of the low pressure stage.
5. In a multi-stage reciprocating piston type refrigera- References (Iited in the file of this patent UNITED STATES PATENTS 578,499 920,421 Boland May 4, 1909 1,746,394 Guild -Feb. 11, 1930- FOREIGN PATENTS 147,244 Switzerland Aug. 1, 1931 Pierson Mar. 9, 1897

Claims (1)

1. THE SYSTEM FOR MINIMIZING LUBRICATING OIL LOSS IN A MULTI-STAGE RECIPROCATING PISTON GAS COMPRESSOR HAVING AT LEAST ONE HIGH PRESSURE STAGE AND ONE LOW PRESSURE STAGE PROVIDED WITH A CRANKCASE, WHICH COMPRISES, CONDUIT MEANS INTERCONNECTING THE DISCHARGE OF SAID LOW PRESSURE STAGE WITH THE HIGH PRESSURE STAGE CRANKCASE AND CONDUIT MEANS ALSO INTERCONNECTING SAID CRANKCASE WITH THE SUCTION ZONE OF SAID LOW PRESSURE STAGE OF THE COMPRESSOR TO INDUCE THE OIL TO FLOW FROM SAID LOW PRESSURE STAGE DISCHARGE INTO THE CRANKCASE.
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Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3514221A (en) * 1967-06-07 1970-05-26 Commissariat Energie Atomique Pump
US3976400A (en) * 1975-03-03 1976-08-24 Altex Scientific, Inc. Gradient pump apparatus
US4396363A (en) * 1980-09-16 1983-08-02 Nippon Piston Ring Co., Ltd. Small reciprocating pump
US20030215339A1 (en) * 2002-05-20 2003-11-20 Grimmer John E. Multi-stage gas compressor system
US20150361972A1 (en) * 2013-02-27 2015-12-17 Bitzer Kuehlmaschinenbau Gmbh Refrigerant compressor system

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US578499A (en) * 1897-03-09 Compressor for refrigerating-machines
US920421A (en) * 1908-04-11 1909-05-04 William J Boland Gas-compressor.
US1746394A (en) * 1927-11-05 1930-02-11 Herbert C Guild Multistage compressor
CH147244A (en) * 1930-06-18 1931-05-31 Baumann Carl Compressors for refrigeration systems with stepped pistons.

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US578499A (en) * 1897-03-09 Compressor for refrigerating-machines
US920421A (en) * 1908-04-11 1909-05-04 William J Boland Gas-compressor.
US1746394A (en) * 1927-11-05 1930-02-11 Herbert C Guild Multistage compressor
CH147244A (en) * 1930-06-18 1931-05-31 Baumann Carl Compressors for refrigeration systems with stepped pistons.

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3514221A (en) * 1967-06-07 1970-05-26 Commissariat Energie Atomique Pump
US3976400A (en) * 1975-03-03 1976-08-24 Altex Scientific, Inc. Gradient pump apparatus
US4396363A (en) * 1980-09-16 1983-08-02 Nippon Piston Ring Co., Ltd. Small reciprocating pump
US20030215339A1 (en) * 2002-05-20 2003-11-20 Grimmer John E. Multi-stage gas compressor system
US6695591B2 (en) * 2002-05-20 2004-02-24 Grimmer Industries, Inc. Multi-stage gas compressor system
US20150361972A1 (en) * 2013-02-27 2015-12-17 Bitzer Kuehlmaschinenbau Gmbh Refrigerant compressor system

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