US3168236A - Oil scavenging system for a rotary compressor - Google Patents

Oil scavenging system for a rotary compressor Download PDF

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Publication number
US3168236A
US3168236A US306760A US30676063A US3168236A US 3168236 A US3168236 A US 3168236A US 306760 A US306760 A US 306760A US 30676063 A US30676063 A US 30676063A US 3168236 A US3168236 A US 3168236A
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Prior art keywords
manifold
oil
pressure
line
compressor
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Expired - Lifetime
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US306760A
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English (en)
Inventor
Ralph E Lamberton
Orville R Lowther
Robert A Redding
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Jaeger Machine Co
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Jaeger Machine Co
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Priority to US306760A priority Critical patent/US3168236A/en
Priority to GB29264/64A priority patent/GB1007236A/en
Priority to CH1048164A priority patent/CH415930A/fr
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Publication of US3168236A publication Critical patent/US3168236A/en
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Assigned to UNITED STATES DEPARTMENT OF COMMERCE, ECONOMIC DEVELOPMENT ADMINISTRATION THE reassignment UNITED STATES DEPARTMENT OF COMMERCE, ECONOMIC DEVELOPMENT ADMINISTRATION THE SECURITY INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: JAEGER MACHINE COMPANY, THE
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C28/00—Control of, monitoring of, or safety arrangements for, pumps or pumping installations specially adapted for elastic fluids
    • F04C28/24—Control of, monitoring of, or safety arrangements for, pumps or pumping installations specially adapted for elastic fluids characterised by using valves controlling pressure or flow rate, e.g. discharge valves or unloading valves
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C28/00—Control of, monitoring of, or safety arrangements for, pumps or pumping installations specially adapted for elastic fluids
    • F04C28/06—Control of, monitoring of, or safety arrangements for, pumps or pumping installations specially adapted for elastic fluids specially adapted for stopping, starting, idling or no-load operation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C28/00—Control of, monitoring of, or safety arrangements for, pumps or pumping installations specially adapted for elastic fluids
    • F04C28/28—Safety arrangements; Monitoring
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
    • F04C29/0007—Injection of a fluid in the working chamber for sealing, cooling and lubricating
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04C—ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; ROTARY-PISTON, OR OSCILLATING-PISTON, POSITIVE-DISPLACEMENT PUMPS
    • F04C29/00—Component parts, details or accessories of pumps or pumping installations, not provided for in groups F04C18/00 - F04C28/00
    • F04C29/02—Lubrication; Lubricant separation
    • F04C29/026—Lubricant separation

Definitions

  • Cur invention relates to an oil scavenging system for a rotary compressor. It relates, more particularly, to an oil scavenging system for a multi-stage rotary compressor having an interstage manifold connecting the highpressure and low-pressure cylinders and having an oilsupplying pressure system connected to the cylinders.
  • the present invention constitutes an improvement over the oil-scavenging system disclosed and claimed in the patent to Lamberton No. 2,739,758, issued March 27, 1956.
  • a scavenging system connected with the interstage manifold, for preventing the accumulation of an excessive amount of oil in the manifold, during unloaded periods, which might interfere with the proper operation of the compressor when again loaded and cause damage to parts of the compressor, such as to the rotor blades thereof.
  • the scavenging system of this invention comprises means for creating a jet of fluid, either air, oil, or a mixture of oil and air, which is connected to the manifold and which jets the fluid through the manifold, during the unloaded cycle, in the direction of normal flow through the manifold thereby scavenging therefrom any oil tending to accumulate therein so as to prevent increase of the oil level therein to a dangerous extent.
  • FIGURE 1 is a plan view of a two-stage compressor showing one scavenging system according to our invention applied thereto.
  • FIGURE 2 is a side elevational view, partly broken away, of the compressor with the scavenging system applied thereto.
  • FIGURE 3 is a broken away, perspective view illustrating the compressor cylinders and connected interstage manifold and the scavenging system of our invention associated therewith.
  • FIGURE 4 is an enlarged vertical sectional view, taken along line 4-4- of FIGURE 2, through the unloading valve of the compressor.
  • FIGURE 4a is a view similar to FIGURE 4 but showing a connection thereto of another scavenging system according to our invention.
  • FIGURE 5 is a schematic View of the scavenging systern shown in FIGURES l to 3, and illustrating its connections to the compressor unit.
  • FIGURE 6 is a similar schematic view of another form of a scavenging system according to our invention connected to the unloader valve as, in FIGURE 4a.
  • FIGURE 7 is a similar view of still another form of scavenging system according to our invention.
  • FIGURE 8 is a schematic view of an additional form of scavenging system embodying our invention.
  • FIGURE 9 is a schematic view of another variation of a scavenging systemaccording to our invention.
  • our invention is applicable to the type of rotary compressor illustrated in the patent to Lamberton No. 2,739,758, issued March 27, 1956.
  • an oil scavenging system for a similar purpose but the present invention provides a number of improvements over that system.
  • the present invention operates on a fluid-jet principle provided by proper connections in the system between a source of fluid under pressure, such as air, oil, or an air-oil mixture, and the interstage manifold to provide a jet of fluid through the manifold while the compressor is unloaded, in the direction of normal fluid flow through the manifold, to force therefrom any oil tending to accumulate therein and thereby prevent undue accumulation thereof during the unloaded period.
  • a source of fluid under pressure such as air, oil, or an air-oil mixture
  • This will prevent oil entering the high-pressure cylinder, upon loading of the compressor, in a volume or mass sufiicient to completely or nearly fill the space between two vanes of the high-pressure rotor and thereby possibly damage it.
  • FIG. 1 An example of a multi-stage rotary compressor of the type to which our invention is applicable is illustrated in the drawings. It is shown as being of the two-stage type and as including a low-pressure cylinder 11 and a high-pressure cylinder 12. These cylinders are shown connected together at their lower sides by an interstage manifold 13 so that the low-pressure air discharged from the cylinder 11 will be conducted into the cylinder 12 for further compression but it is possible to have the manifold built-in into the cylinders.
  • the low-pressure cylinder 11 (FIGURE 3) houses the rotor 14 which is driven from a suitable engine (not shown) coupled to the rotor-driving gear 14a.
  • the rotor 14 is coupled to and drives the rotor 15 which is housed in the high-pressure cylinder 12.
  • the low-pressure cylinder is provided with the valve-controlled air inlet 16.
  • the high-pressure cylinder 12 is provided with a discharge outlet which connects by a discharge line 17 to the airreceiver 18 (FIGURE 5) of the compressor.
  • This airreceiver 13 will have the usual oil reservoir tank 19 and oil separator 20 connected thereto.
  • the ing pump 21 which is coupled to the high-pressure rotor '15 so that it is driven thereby.
  • This pump may be an oil-gear type or any other suitable type.
  • the oil supplied from the dischar e line 22 of the pump to the various parts by the pressure systems serves as a lubricant, a sealing agent, and for cooling.
  • the oil supplied to the lowpressure cylinder 11 passes therefrom, with the air compressed therein, through the interstage manifold 13 to the high-pressure cylinder 12. This air, bearing a supply of oil, is further compressed in the cylinder 12 and is discharged through the line 17 into the air-receiver 18.
  • substantially all oil supplied to each cylinder 11 and 12 is carried along by the velocity of the air.
  • the compressor air inlet 16 is controlled by a common type of unloading valve unit 3th, a suitable valve unit being illustrated in FIGURE 4. It comprises a pistonttype valve member 31 which is pressure-actuated.v This valve member 31 is disposed in a housing 32 mounted on the low-pressure cylinder 11 over the inlet 16 and communicating therewith.
  • the housing is provided with an inlet collar portion 33 leading thereinto and having a valve seat 34 at its inner end with which the valve member 31 cooperates.
  • a filter unit 35 is mounted on the outer end of the inlet collar portion 33. Atmospheric air will be drawn through the filter unit 35 and be filtered before it enters the housing 32 through the inlet collar portion 33.
  • Air for operating the valve 39 will be supplied when a predetermined pressure is reached in the receiver side of the compressor through a pressure-relief valve 36 which is connected thereto by a line 37.
  • the valve 36 is connected to the receiver side of the compressor by a line 38 which, in the example shown, is connected to the air service outlet line between the discharge end of the separator 20 and a check valve 29 in that line, as shown in FIGURE 5.
  • the valve 36 may take various for-ms but a suitable type is shown in FIGURE 3.
  • the inlet line 38 leads into an inlet passage 39 which is controlled by a diaphragmcarried, semi-spherical valve member 40 normally held on its seat by an adjustable spring 41.
  • An outlet passage 42 leads from the valve into the line 37.
  • valve member 443 When receiver pressure, exerted through the separator 20, reaches a predetermined extent, the valve member 443 is unseated and the air under pressure reaches the line 37 through the outlet 42. This pressure will seat the un loading valve member 31 and the valve 36 may be adjusted to vary the actuating pressure.
  • a vent 43 allows some of the air to escape from the inlet valve piston chamber as closing pressure is supplied in order to modulate the closing movement.
  • the oil passing from the low-pressure cylinder 11 with the air will pass into the high-pressure cylinder 12 and out to the air receiver 18.
  • the interstage manifold 13 will be at a much lower pressure than the oil separator 20.
  • the compressor is loaded, the oil passing from the low-pressure cylinder 11 with the air will pass into the high-pressure cylinder 12' and out to the air receiver 18.
  • the compressed air flows from the .treceiver 18 into the separator 29 and any oil vapors remaining in the air are retained in the filtering elements in the oil separator and are passed from the separator into the drain line 24.
  • the check valve 26 in the line '24 will prevent oil from being forced back up into the separator when the compressor is started. As soon,
  • connection of the line 24 to the interstage manifold 13 will prevent the accumulation of oil in the manifold when the compressor is running unloaded at which time there is a tendency for oil to accumulate in the manifold since there is very little ,air in circulation within the compressor at this time, due
  • outlet end of the line 24 is connected to the upstream end of the manifold preferably directly over the bottom wall thereof, as shown best in FIGURES 2 and 3.
  • the inlet end of the line 24 is connected to the separator 28 at the lowest point adjacent the air discharge end of the separator 20, as shown in FIGURE 5.
  • the air compressor is a portable compressor and is used for work on very irregular terrain, the compressor may be operating at very steep angles which could possibly cause an excessive accumulation of oil in the lowest end of the manifold with resulting serious damage or breakage of the vanes of the rotor 15 in the high-pressure cylinder.
  • the oil tank 19, the receiver 18 and the separator 20 are shown as separate tanks but it is to be understood that the oil could collect in the bottom of the receiver tank so that the separate oil tank l9-could be eliminated. Also, the oil separator tank could be disposed within the receiver tank. Our scavenging system would work equally well with such modifications of the compressor system.
  • FIGURE 6 A somewhat different but efiective scavenging system, in accordance with our invention, is illustrated diagrammatically in FIGURE 6.
  • the line 38a from the separator 26a serves both as a pressure line for actuating the inlet valve 30a and as a bleed line from the separator.
  • This line is connected to the inlet side of the pressure relief valve 36a which is connected by the line 37a to the actuating chamber of the valve 30a, as indicated in FIGURE 4a.
  • An oil-scavenging line .24a leads from this actuating chamber to the manifold 130.
  • This oil-scavenging line has the filter 25a, the
  • the scavenging jet producing fluid will first pass through the valves 66a and 3% before reaching the manifold 13a.
  • the air and oil mixture from the separator 20a does not reach the manifold 13a since the flow is interrupted at the closed valve 36a.
  • the valve 36a is opened, allowing the air and oil mixture to flow into the actuating chamber of the inlet valve 30a, opening it, and flowing on through the line 24a into the manifold 13a.
  • valve 30a is actuated to unload the compressor and simultaneously the scavenging jet is created in the manifold 13a. This jet will continue to function as long as the compressor is operating in the unloaded state.
  • the valve 36a will close, permitting the valve 30a to open, causing the compressor to again be loaded, and simultaneously interrupting the scavenging jet through the line 24a.
  • FIGURE 7 Still another form of oil-scavenging system embodying our invention is illustrated in FIGURE 7.
  • This system is similar to that illustrated in FIGURE except that a pump is used in the jet-producing line to increase the pressure of the fluid therein.
  • the bleed line 24b runs from the separator b to the inlet side of a pump 24g and then on to its connection with the manifold 13b at the upstream side thereof, as before.
  • This line 2412 has the filter 25b, the check valve 26b, and the choke 27b connected therein as before.
  • the pump 245 may be of a type similar to the pump 21b adjacent to which it may be mounted and it may be driven by the same drive from the high-pressure rotor shaft.
  • the inlet valve 30b will be actuated by the valve 36!; which is connected to the separator 26b by a line 3811, as in the example shown in FIGURE 5.
  • the oil scavenging jet will function exactly the same as that described with reference to FIGURE 5 but the pressure of the fluid discharged into the upstream end of the manifold 1317 will be increased by the pump 24g.
  • FIGURE 8 illustrates another form of scavenging system according to our invention. This is identical with the system shown in FIGURE 6 except that an additional scavenging line is provided to the manifold.
  • the additional line 38c leads from the air service outlet line between the outlet end of the separator 20c and the check valve 290 provided in that line and connects to the actuating chamber of the inlet valve 3% through the valve 360 and the line 37c.
  • An oilscavenging line 240 leads from this actuating chamber to the upstream end of the manifold 130. This line has the filter 250, the check valve 260, and the choke (not shown) therein.
  • the drain or bleed line 24d from the oil separator 29c also serves as a scavenging line and connects to the upstream end of the manifold 130 adjacent the bottom thereof side-by-side with the line 240.
  • This line has the filter 25d, the check valve 26d, and the choke 27d connected therein.
  • This line will function the same as the line 24 in FIGURE 5, to provide a jet of oil and air mixture into the upstream end of the manifold.
  • the line 240 will function to provide an additional jet of practically oil-free air into the upstream end of the manifold, directed toward the downstream end thereof.
  • the two jets directed sideby-side will serve effectively to prevent accumulation of oil in the manifold 130.
  • FIGURE 9 The arrangement illustrated in FIGURE 9 is similar to the one just described including the air line 38c, valve 36c, line 37a, valve 30e, and scavenging line 24e connected to the upstream end of the manifold 13c.
  • the bleed or drain line 24 runs from the bottom of the separator 20a to the inlet 16c of the low-pressure cylinder.
  • the scavenging line 24c will function exactly the same as the line 240 in FIG- URE 8 to provide a jet of air in the upstream end of the manifold 13c directed toward the downstream end thereof to prevent accumulation of oil in the manifold.
  • This system comprises means for creating a jet or jets of fluid directed into the manifold at the upstream end thereof toward the downstream end thereof in the direction of the normal flow from the low-pressure cylinder to the high-pressure cylinder and will, therefore, prevent the accumulation of oil therein which tends to occur during the unloaded operation of the compressor.
  • the jet of fluid is produced by a pressure difierential created by proper connections from the receiver or high-pressure side of the compressor to the lower pressure manifold. This jet of fluid will move any oil tending to accumulate in the manifold toward the inlet of the high-pressure cylinder.
  • a multi-stage rotary compressor having a high-pressure side including a high-pressure cylinder and a low-pressure side including a low-pressure cylinder and an interstage manifold connecting the high and low pressure cylinders thereof and having a highpressure oil lubricating system connected to the cylinders
  • interstage manifold has an upstream end connected to the low-pressure cylinder and a downstream end connected to the high-pressure cylinder, said line having a discharge end extending into the upstreamend of the manifold at ti? lower side thereof toward said downstream end there- 0 7.
  • the interstage manifold has an upstream end connected to the low-ipressure cylinder and a downstream end connected to the high-pressure cylinder, said line being connected to the upstream end of the manifold, and a pressure-relief valve in the line for controlling the flow through said line into said manifold.
  • the interstage manifold has an upstream end connected to the low-pressure cylinder and a downstream end connected to the high-pressure cylinder, said line being connected to the upstream end of the manifold, an inlet valve connected to the low-pressure cylinder, an additional line running from the separator at its discharge side to said inlet valve through :a pressure relief valve, and a line running from said inlet valve to the upstream end of the manifold.
  • the interstage manifold has an upstream end connected to the low-pressure cylinder and a downstream end connected to the high-pressure cylinder, said low pressure cylinder having an inlet, said line being connected to said lowpressure cylinder at said inlet, an inlet valve connected to said low-pressure cylinder at said inlet, an additionalline running from the separator at its discharge side to said inlet valve, and a line running from said inlet valve to the upstream end of the manifold.
  • a multi-stage rotary compressor with an interstage manifold and a high-pressure oil supply system including an oil separator, said manifold having an inlet upstream end, an outlet downstream end and a fluid line leading from the separator and connected to the upstream 8 end of the manifold to supply a jet of fluid under pressure toward the downstream end of the manifold to aid removing :oil therefrom.
  • a multi-stage rotary compressor having 'a manifold, a low-pressure stage and a high-pressure stage with the manifold leading from the low-pressure stage to the high-pressure stage, said manifold having an upstream end connected to the low-pressure stage and a downstream end connected to the high-pressure stage and a high-pressure oil-supply system for the stages, means for preventing the accumulation of excessive amounts of oil in the manifold, said means comprising a fluid connection between the high-pressure stage and the upstream end of the manifold for directing a jet of fluid therein toward the'd-ownstream end of the manifold.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Rotary Pumps (AREA)
  • Applications Or Details Of Rotary Compressors (AREA)
US306760A 1963-09-05 1963-09-05 Oil scavenging system for a rotary compressor Expired - Lifetime US3168236A (en)

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US306760A US3168236A (en) 1963-09-05 1963-09-05 Oil scavenging system for a rotary compressor
GB29264/64A GB1007236A (en) 1963-09-05 1964-08-04 Oil scavenging system for a rotary compressor
CH1048164A CH415930A (fr) 1963-09-05 1964-08-11 Compresseur rotatif

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Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3448916A (en) * 1967-06-16 1969-06-10 Ingersoll Rand Co Unloading system for compressors
US3632231A (en) * 1970-02-19 1972-01-04 Worthington Corp Suction pressure relieving system for a rotary vane compressor
US3778192A (en) * 1972-04-07 1973-12-11 Davey Compressor Method and apparatus for unloading a rotary compressor
US3788776A (en) * 1972-08-10 1974-01-29 Gardner Denver Co Compressor unloading control
US3936249A (en) * 1973-11-26 1976-02-03 Hokuetsu Kogyo Co., Ltd. Rotary compressor of oil cooling type with appropriate oil discharge circuit
US4089623A (en) * 1975-01-02 1978-05-16 Sullair Schraubenkompressoren Gmbh Compressor intake control
US4123203A (en) * 1977-10-14 1978-10-31 Gardner-Denver Company Multistage helical screw compressor with liquid injection
US4483667A (en) * 1981-12-17 1984-11-20 Leybold-Heraeus Gmbh Vacuum pump and method of operating the same
US4655698A (en) * 1985-07-26 1987-04-07 The United States Of America As Represented By The Secretary Of The Navy Compressor-scavenging eductor system
EP0478939A3 (en) * 1990-10-03 1992-04-22 Ing. Enea Mattei S.P.A. Two-stage rotary compressor for refrigerating plants
US5667367A (en) * 1994-04-08 1997-09-16 Kabushiki Kaisha Kobe Seiko Sho Air compressor
US20160290521A1 (en) * 2013-06-28 2016-10-06 GEA AWP GmbH Non-return valve/filter unit
US20160290693A1 (en) * 2013-11-25 2016-10-06 The Coca-Cola Company Compressor with an Oil Separator
US11506082B2 (en) 2019-01-23 2022-11-22 Rolls-Royce Plc Oil scavenge system

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8809621D0 (en) * 1988-04-22 1988-05-25 Boc Group Plc Dry pump with closed loop filter
EP0863313A1 (fr) * 1997-03-04 1998-09-09 Anest Iwata Corporation Compresseur à volutes à deux étages

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2739758A (en) * 1955-03-23 1956-03-27 Jaeger Machine Co Rotary compressor

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2739758A (en) * 1955-03-23 1956-03-27 Jaeger Machine Co Rotary compressor

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3448916A (en) * 1967-06-16 1969-06-10 Ingersoll Rand Co Unloading system for compressors
US3632231A (en) * 1970-02-19 1972-01-04 Worthington Corp Suction pressure relieving system for a rotary vane compressor
US3778192A (en) * 1972-04-07 1973-12-11 Davey Compressor Method and apparatus for unloading a rotary compressor
US3788776A (en) * 1972-08-10 1974-01-29 Gardner Denver Co Compressor unloading control
US3936249A (en) * 1973-11-26 1976-02-03 Hokuetsu Kogyo Co., Ltd. Rotary compressor of oil cooling type with appropriate oil discharge circuit
US4089623A (en) * 1975-01-02 1978-05-16 Sullair Schraubenkompressoren Gmbh Compressor intake control
US4123203A (en) * 1977-10-14 1978-10-31 Gardner-Denver Company Multistage helical screw compressor with liquid injection
US4483667A (en) * 1981-12-17 1984-11-20 Leybold-Heraeus Gmbh Vacuum pump and method of operating the same
US4655698A (en) * 1985-07-26 1987-04-07 The United States Of America As Represented By The Secretary Of The Navy Compressor-scavenging eductor system
EP0478939A3 (en) * 1990-10-03 1992-04-22 Ing. Enea Mattei S.P.A. Two-stage rotary compressor for refrigerating plants
US5667367A (en) * 1994-04-08 1997-09-16 Kabushiki Kaisha Kobe Seiko Sho Air compressor
US20160290521A1 (en) * 2013-06-28 2016-10-06 GEA AWP GmbH Non-return valve/filter unit
US20160290693A1 (en) * 2013-11-25 2016-10-06 The Coca-Cola Company Compressor with an Oil Separator
US10309704B2 (en) * 2013-11-25 2019-06-04 The Coca-Cola Company Compressor with an oil separator between compressing stages
US11506082B2 (en) 2019-01-23 2022-11-22 Rolls-Royce Plc Oil scavenge system

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Publication number Publication date
CH415930A (fr) 1966-06-30
GB1007236A (en) 1965-10-13

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Owner name: UNITED STATES DEPARTMENT OF COMMERCE,ECONOMIC DEVE

Free format text: SECURITY INTEREST;ASSIGNOR:JAEGER MACHINE COMPANY, THE;REEL/FRAME:003954/0254

Effective date: 19810224

Owner name: UNITED STATES DEPARTMENT OF COMMERCE, ECONOMIC DEV

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Effective date: 19810224