US2646212A - Oil level equalizing device for multiple compressor arrangement - Google Patents

Oil level equalizing device for multiple compressor arrangement Download PDF

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US2646212A
US2646212A US19844750A US2646212A US 2646212 A US2646212 A US 2646212A US 19844750 A US19844750 A US 19844750A US 2646212 A US2646212 A US 2646212A
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housing
compressor
oil
crankcase
reservoir
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Edward P Kellie
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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B39/00—Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
    • F04B39/12—Casings; Cylinders; Cylinder heads; Fluid connections
    • F04B39/128—Crankcases
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04B—POSITIVE-DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS
    • F04B39/00—Component parts, details, or accessories, of pumps or pumping systems specially adapted for elastic fluids, not otherwise provided for in, or of interest apart from, groups F04B25/00 - F04B37/00
    • F04B39/02—Lubrication
    • F04B39/0207—Lubrication with lubrication control systems
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B31/00—Compressor arrangements
    • F25B31/002—Lubrication
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25—REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25B—REFRIGERATION MACHINES, PLANTS OR SYSTEMS; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS
    • F25B1/00—Compression machines, plants or systems with non-reversible cycle
    • F25B1/10—Compression machines, plants or systems with non-reversible cycle with multi-stage compression
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/7287—Liquid level responsive or maintaining systems
    • Y10T137/7358—By float controlled valve
    • Y10T137/7439—Float arm operated valve
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00—Fluid handling
    • Y10T137/8593—Systems
    • Y10T137/85978—With pump
    • Y10T137/86131—Plural
    • Y10T137/86139—Serial

Definitions

  • This invention relates to an oil level equalizing device for multiple compressor arrangement.
  • Lubrica-- tion of all the mechanical parts is necessary. Lubricating oil is circulated through, the com- I8.
  • line 20 is optional but is preferred because it maintains equal the gaseous pressure in crankcase 3 and housing 8;
  • Pipe line or tube H 2i connects the crank case 4 with port 22111 pressor and valves.
  • low temperature refrigeration systems where the refrigerant is compressed in two or more stages, it is an established fact that all the oil will tend to migrate into the crankcase of one compressor.
  • the low stage suction line or tube I3 connects the evaporator I with the intake port of compressor 4.
  • the low stage compression discharge w line or tube I4 connects the outlet port of compressor 4 with the suction or intake port of the high stage compressor I.
  • High stage compression discharge line I5 connects the exhaust'port of compressor I with the oil separator 5 wherein the lubricating oil is separated from the com pressed refrigerant in a wellknown manner.- The use of oil separator 5 is preferred butoptional.
  • Tube or line I6 conducts the highly compressed gaseous refrigerant from the oil separator to the condenser-
  • the oil-which is separated from the gaseous refrigerantin separator 5 returns from the separator 5 through pipe line or tube I'I- to the crankcase of high stage compressor I.
  • the oil level in crankcase 3 is indicated by the dotted line l8.
  • the crankcase 3 is connected by 7 housing 8.
  • - Port 22 is preferably located in the bottom of housing 8 but in any event below the oil level 23 in housing 8.
  • the oil level in crank case 4 is indicated by the'dotted line 24.
  • the instant oil level equalizing device is shown incorporated in a multiple stage refrigeration system only for purposes of description and not by wayof limitation:
  • the instant oil level equalizing device can be used in any multiple compressor system.
  • the operation of. the multiple stage low temperature refrigeration system is conventional and will only be described briefly.
  • the gas entering compressor 2 throughthe low stage suction line is compressed and discharged through line I4 into high stage-compressor I where this refrig-- erant is compressed to a higher pressure and then discharged through line I5 into oil separator 5 where the oil is separated from the gaseous refrigerant.
  • the compressed gaseous refrigerant passes along line I6 into condenser 6 where it is cooled and condensed to a liquid state.
  • the liquid refrigerant passes through capillary or restrictor tube I2 to evaporator I where it evaporates and takes up heat in a Well known manner to efiect refrigeration:
  • compressors I- and 2- are positioned at the same level but itisunderstood that either of compressors I and 2 can be positioned on a higher level than the other.
  • the entire system isa closed system and the crankcases 3 and 4 and" the valve housing 8 are pressure and vacuum tight;
  • the float valve arrangement shown will maintain the oil in the crankcase housings 3 and 4 of the compressors equal or at the same level,
  • crankcases 3 and 4 are operating at different pressures and. even though the compressorsare located at different levels.
  • Valve housing 8 is preferably made in two sections 25 and 26, the upper section 26- being telescoped within section 25.
  • the junction line 28 on the outside of housings 25 and 26 serves as a calibration indicating the level 23 at which float valve I I will open. If the pressure in crankcase 3 is higher than that in crankcases (irrespective of whether crankcase 3 is positioned at a higher or lower level thancrankcase 4), then calibrated opening line 2
  • crankcase 4 will be ported to suction line l3 and maintained at the same pressure as suctionline l3 and crankcase 3 will be ported to suction line I l and maintained at the same pressure as suction line I4. Also any oil removed from the crankcase 4 of compressor 2'will'bedischarged to compressor 1. The oil discharged from compressor I through line will be separated in separator 5 and returned to crankcase 3 through. line I1.
  • crankcase 3 The return of oil through line ll to crank case 3 tends to raise the oil level 18 in this crankcase. Since the oil in housing 8 and crankcase 3 is under the same pressure, it will flow from crankcase 3 into housing 8 tending to make the oil levels in housing 8 and crankcase 3 equal. As the oil returns t crankcase 3 through line H and raises oil level 18 it raises the oil level 23 in housing 8 a like amount until level 23 has raised to the point at which float 9 opens needle valve H so that oil can now flow from housing 8 through line 21 into crankcase 4.
  • crankcase 3 When the oil ceases to flow from the separator 5 into crankcase I the oil level stabilizesat its proper point and the float 9 closes needle valve ll thereby preventing furtherflow of oil through line 2i to crankcase 4 and this closing of valve ll isolates crankcase 4 from crankcase 3. In this way the pressure in crankcase 3 can be maintained at a higher pressure than that in crankcase 4.
  • H3, II will prevent the migration of all the oil into one compressor and at the same, time permit a difierence in pressures in the difierent I crankcases.
  • each compressor having a reservoir for 3.
  • The-combination claimed in claim 2 wherein the reservoir of the higher stage compressor-is maintained at a pressure higher than the reser-' voir of the lower stage compressor.
  • each compressor having a reservoir for-liquid lubricant, a housing, a liquid conducting linebetween the lower portion of said housing and the lower portion of the reservoir of said higher stage compressor, a fluid conducting linev connecting the upper portion of said housing with the upper portion of the reservoir of said higher stage compressor whereby the gaseous pressures in said housing and reservoir are equalized, a
  • the reservoir for the higher stage compressor being maintained at a higher pressure thanthe reservoir for the lower-stage compressor, a housing, a liquid conducting line connecting the lower portion of said housing with the lower portion of the reservoir of said higher stage compressor,
  • a fluid conducting line connecting the upper portion of the housing with the upper portion of the reservoir of the higher stage compressor whereby the gaseous pressures in. said housing and said last mentioned reservoir are equalized, said housing being disposed at substantially the same level as said last mentioned reservoir and the liquid conducting line between said housing and said last mentioned reservoir being open whereby the liquid lubricant levels in said housing and said last mentioned reservoir will equalize, a liquid conducting line connecting said housing with the reservoir of the lower stage compressor, a valve for controlling the flow through said last mentioned liquid conducting line, means responsive to the liquid level in said 6 housing for closing said valve when the level of the liquid in the reservoir in the higher stage compressor is at or below a desired normal level, and means in circuit with said higher stage compressor for separating the lubricant in the fluid discharged from said higher stage compressor, said last mentioned means being connected with the reservoir of the higher stage compressor for returning the separated lubricant to'the reservoir of the higher stage compressor.

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
  • Compressor (AREA)

Description

July 21, 1953 2,646,212
E. P. KELLIE OIL LEVEL EQUALIZING DEVICE FOR MULTIPLE COMPRESSOR ARRANGEMENT Filed NOV. 30, 1950 Evaporo for Cop/Wary Ii/be,
Condenser INVENTOR. Edward P Kellie l atented July 21 195 3 OIL LEVEL EQUALIZING DEVICE FOR MULTF PLE COMPRESSOR ARRANGEMENT Edward '1 Kellie, Detroit, Mich;
Application November 30, 1950, Serial No; 198,447
v 5 Claims. 1 This invention relates to an oil level equalizing device for multiple compressor arrangement.
In a mechanical refrigeration system lubrica-- tion of all the mechanical parts is necessary. Lubricating oil is circulated through, the com- I8. The use of line 20 is optional but is preferred because it maintains equal the gaseous pressure in crankcase 3 and housing 8; Pipe line or tube H 2i connects the crank case 4 with port 22111 pressor and valves. In low temperature refrigeration systems where the refrigerant is compressed in two or more stages, it is an established fact that all the oil will tend to migrate into the crankcase of one compressor.
It is an object of this invention to produce an oil level equalizing device which will tend to maintain equal the oil levels in the crankcases of a multiple compressor system irrespective of whether the compressors are located at the same vor different levels and irrespective of whether comprising the following elements reciprocating piston type compressors I and 2 provided with crankcases 3 and 4, oil separator 5, condenser 6, evaporator l, float valve housing 8, float 9 pivoted as at I within housing 8, valve II, a metering device such as capillary or restrictor tube I2 lo'etween condenser 6 and evaporator I.
The low stage suction line or tube I3 connects the evaporator I with the intake port of compressor 4. The low stage compression discharge w line or tube I4 connects the outlet port of compressor 4 with the suction or intake port of the high stage compressor I. High stage compression discharge line I5 connects the exhaust'port of compressor I with the oil separator 5 wherein the lubricating oil is separated from the com pressed refrigerant in a wellknown manner.- The use of oil separator 5 is preferred butoptional. Tube or line I6 conducts the highly compressed gaseous refrigerant from the oil separator to the condenser- The oil-which is separated from the gaseous refrigerantin separator 5 returns from the separator 5 through pipe line or tube I'I- to the crankcase of high stage compressor I. The oil level in crankcase 3 is indicated by the dotted line l8. The crankcase 3 is connected by 7 housing 8.- Port 22 is preferably located in the bottom of housing 8 but in any event below the oil level 23 in housing 8. The oil level in crank case 4 is indicated by the'dotted line 24.
The instant oil level equalizing device is shown incorporated in a multiple stage refrigeration system only for purposes of description and not by wayof limitation: The instant oil level equalizing device can be used in any multiple compressor system. Y
The operation of. the multiple stage low temperature refrigeration system is conventional and will only be described briefly. The gas entering compressor 2 throughthe low stage suction line is compressed and discharged through line I4 into high stage-compressor I where this refrig-- erant is compressed to a higher pressure and then discharged through line I5 into oil separator 5 where the oil is separated from the gaseous refrigerant. The compressed gaseous refrigerant passes along line I6 into condenser 6 where it is cooled and condensed to a liquid state. The liquid refrigerant passes through capillary or restrictor tube I2 to evaporator I where it evaporates and takes up heat in a Well known manner to efiect refrigeration:
As shown, compressors I- and 2- are positioned at the same level but itisunderstood that either of compressors I and 2 can be positioned on a higher level than the other. The entire system isa closed system and the crankcases 3 and 4 and" the valve housing 8 are pressure and vacuum tight; The float valve arrangement shown will maintain the oil in the crankcase housings 3 and 4 of the compressors equal or at the same level,
I8 and 24, even though the crankcases 3 and 4 are operating at different pressures and. even though the compressorsare located at different levels.
Valve housing 8 is preferably made in two sections 25 and 26, the upper section 26- being telescoped within section 25. The junction line 28 on the outside of housings 25 and 26 serves as a calibration indicating the level 23 at which float valve I I will open. If the pressure in crankcase 3 is higher than that in crankcases (irrespective of whether crankcase 3 is positioned at a higher or lower level thancrankcase 4), then calibrated opening line 2| should be positioned in thehorizontalplane of the correct oil level I8' which it is desired to maintain in crankcase liquid lubricant, a housing, a liquid conducting 3. If the gaseous pressures in crankcases 3 and 4 are the same but crankcase 4 is positioned at a higher level than crankcase 3, then the calibrated opening point or-line 28 should be positioned in the horizontal plane of the oil level of the higher located crankcase 4.
In the operation of the above system .any oil returning to compressor 2 with the gaseous refrigerant through line [3 will or may be in part retained in compressor crankcase 4 andin part discharged with the low stage compressed gas through line l4 into compressor I. If desired, in accord with conventional practice, crankcase 4 will be ported to suction line l3 and maintained at the same pressure as suctionline l3 and crankcase 3 will be ported to suction line I l and maintained at the same pressure as suction line I4. Also any oil removed from the crankcase 4 of compressor 2'will'bedischarged to compressor 1. The oil discharged from compressor I through line will be separated in separator 5 and returned to crankcase 3 through. line I1.
The return of oil through line ll to crank case 3 tends to raise the oil level 18 in this crankcase. Since the oil in housing 8 and crankcase 3 is under the same pressure, it will flow from crankcase 3 into housing 8 tending to make the oil levels in housing 8 and crankcase 3 equal. As the oil returns t crankcase 3 through line H and raises oil level 18 it raises the oil level 23 in housing 8 a like amount until level 23 has raised to the point at which float 9 opens needle valve H so that oil can now flow from housing 8 through line 21 into crankcase 4. When the oil ceases to flow from the separator 5 into crankcase I the oil level stabilizesat its proper point and the float 9 closes needle valve ll thereby preventing furtherflow of oil through line 2i to crankcase 4 and this closing of valve ll isolates crankcase 4 from crankcase 3. In this way the pressure in crankcase 3 can be maintained at a higher pressure than that in crankcase 4.
From the above it is evident-that the instant compressor oil equalizingvalve arrangement 8,
9, H3, II will prevent the migration of all the oil into one compressor and at the same, time permit a difierence in pressures in the difierent I crankcases. r
In installing the oil level equalizing valve arrangement, which is the subject of this invention, it is only necessary to connect. this equalizing valve arrangement into the systemas in dicated and to mount the valve arrangementso that the opening level indicating line 28,15 on, the same level as the correct oil level in the I crankcase to which the inlet side of the housing 8 is connected by line l9, then the correct amount of oil is poured into each crankcase. Thereafter, during the operation of the compressors, oil leaving any crankcase will be. automatically returned in like amount to that crankcase to g 4 line between said housing and the reservoir of said higher stage compressor, a liquid conducting line between said housing and the reservoir of the low stage compressor, said first mentioned liquid line being open whereby the liquid lubricant levels in the reservoir of the higher stage compressor and the housing will equalize, a valve controlling the flow of liquid lubricant from said housing to the reservoir of the lower stage compressor, and means responsive to the liquid level in said housing for opening said valve when the liquid level in said housing rises above a desired normal liquid level in the reservoir of the higher stage compressor whereby the lubricating liquid flows from said housing into the reservoir of the lower stage compressor and the liquid in said reservoirs is maintained at desired levels.
2. The combination claimed in claim 1 includ- -chargep'ort of the higher stage compressor with the separator whereby the liquid lubricant is separatedfrom the compressed gas, and a'fiuid conducting line connecting said separatorwithrator to said last mentioned reservoir.
maintain all the compressor crankcases at theircompressors conducting line connecting the discharge outlet of the lower stage compressor in series with the intake port of the higher stage compressor so that the fluid compressed in the lower-stage compressor is charged into the higher-stage compressor, each compressor having a reservoir for 3. The-combination claimed in claim 2 wherein the reservoir of the higher stage compressor-is maintained at a pressure higher than the reser-' voir of the lower stage compressor.
4. In combination at-least two compressors for compressing gas in multiple stages, a fluid conducting line connecting the discharge outlet of the lower stage compressor in series with the intake port of the higher stage compressor so that the fluid compressed in the lower stage compressor is charged into the higher stage compressor, each compressor having a reservoir for-liquid lubricant, a housing, a liquid conducting linebetween the lower portion of said housing and the lower portion of the reservoir of said higher stage compressor, a fluid conducting linev connecting the upper portion of said housing with the upper portion of the reservoir of said higher stage compressor whereby the gaseous pressures in said housing and reservoir are equalized, a
liquid conducting line between said housing and the reservoir of the. low stage compressor, said. liquid conducting line between said housing and the reservoir. of said higher stage compressor being open and said housing being disposed gen erally at the same :level as the reservoir of said higher stage compressor whereby the liquid lubricant levels in said last mentioned reservoir and the housing will equalize, a valve controlling the flow of liquid lubricant from said housing" to the reservoir of the lowerstage compressonfl and means responsive to the liquid level in said housing foropening said valve when the liquid.-
level in said housingrises above a. desired normal liquid level in the reservoir of the higher stage compressor whereby the lubricating liquid flows from said housing into said reservoir of the: lower stage .compressor and the liquid in said.
reservoirs is maintained at desired levels.-
7 v5. In combination, at least two compressors for compressing gas in multiple stages, a fluid conducting line connecting the discharge outlet.- of the lower. stage compressor with the intake port of the higher stage compressor, each compressor'having' a reservoir for liquid lubricant,
the reservoir for the higher stage compressor being maintained at a higher pressure thanthe reservoir for the lower-stage compressor, a housing, a liquid conducting line connecting the lower portion of said housing with the lower portion of the reservoir of said higher stage compressor,
a fluid conducting line connecting the upper portion of the housing with the upper portion of the reservoir of the higher stage compressor whereby the gaseous pressures in. said housing and said last mentioned reservoir are equalized, said housing being disposed at substantially the same level as said last mentioned reservoir and the liquid conducting line between said housing and said last mentioned reservoir being open whereby the liquid lubricant levels in said housing and said last mentioned reservoir will equalize, a liquid conducting line connecting said housing with the reservoir of the lower stage compressor, a valve for controlling the flow through said last mentioned liquid conducting line, means responsive to the liquid level in said 6 housing for closing said valve when the level of the liquid in the reservoir in the higher stage compressor is at or below a desired normal level, and means in circuit with said higher stage compressor for separating the lubricant in the fluid discharged from said higher stage compressor, said last mentioned means being connected with the reservoir of the higher stage compressor for returning the separated lubricant to'the reservoir of the higher stage compressor.
EDWARD P. KELLIE.
Name Date Gygax Oct. 31, 1939 Number
US19844750 1950-11-30 1950-11-30 Oil level equalizing device for multiple compressor arrangement Expired - Lifetime US2646212A (en)

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Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3015371A (en) * 1959-06-15 1962-01-02 Gits Bros Mfg Co Level regulator
US3719057A (en) * 1971-10-08 1973-03-06 Vilter Manufacturing Corp Two-stage refrigeration system having crankcase pressure regulation in high stage compressor
US4564500A (en) * 1983-10-25 1986-01-14 Westinghouse Electric Corp. Oil pot for reactor coolant pump motor and apparatus for controlling the oil level therein
US4752193A (en) * 1983-09-01 1988-06-21 Bbc Brown Boveri Ltd. Exhaust-gas turbocharger for the two-stage supercharging of an internal-combustion engine with a device to prevent losses of lubricant
US4755110A (en) * 1986-08-11 1988-07-05 Hoerbiger Ventilwerke Aktiengesellschaft Piston-type compressor
WO1997043585A1 (en) * 1996-05-10 1997-11-20 Shaw David N Series connected primary and booster compressors
US5927088A (en) * 1996-02-27 1999-07-27 Shaw; David N. Boosted air source heat pump
US6276148B1 (en) 2000-02-16 2001-08-21 David N. Shaw Boosted air source heat pump
US20050044866A1 (en) * 2003-08-27 2005-03-03 Shaw David N. Boosted air source heat pump
US20060073026A1 (en) * 2004-10-06 2006-04-06 Shaw David N Oil balance system and method for compressors connected in series
US20080173034A1 (en) * 2007-01-19 2008-07-24 Hallowell International, Llc Heat pump apparatus and method
US20140154105A1 (en) * 2012-12-03 2014-06-05 Danfoss (Tianjin) Ltd. Oil balancing apparatus and refrigeration device
US11137180B1 (en) * 2020-04-30 2021-10-05 Trane Air Conditioning Systems (China) Co., Ltd. System and method for OCR control in paralleled compressors

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2178100A (en) * 1937-05-13 1939-10-31 Curtis Refrigerating Machine C Refrigerating condensing unit

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2178100A (en) * 1937-05-13 1939-10-31 Curtis Refrigerating Machine C Refrigerating condensing unit

Cited By (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3015371A (en) * 1959-06-15 1962-01-02 Gits Bros Mfg Co Level regulator
US3719057A (en) * 1971-10-08 1973-03-06 Vilter Manufacturing Corp Two-stage refrigeration system having crankcase pressure regulation in high stage compressor
US4752193A (en) * 1983-09-01 1988-06-21 Bbc Brown Boveri Ltd. Exhaust-gas turbocharger for the two-stage supercharging of an internal-combustion engine with a device to prevent losses of lubricant
US4564500A (en) * 1983-10-25 1986-01-14 Westinghouse Electric Corp. Oil pot for reactor coolant pump motor and apparatus for controlling the oil level therein
US4755110A (en) * 1986-08-11 1988-07-05 Hoerbiger Ventilwerke Aktiengesellschaft Piston-type compressor
US5927088A (en) * 1996-02-27 1999-07-27 Shaw; David N. Boosted air source heat pump
WO1997043585A1 (en) * 1996-05-10 1997-11-20 Shaw David N Series connected primary and booster compressors
US5839886A (en) * 1996-05-10 1998-11-24 Shaw; David N. Series connected primary and booster compressors
US6276148B1 (en) 2000-02-16 2001-08-21 David N. Shaw Boosted air source heat pump
USRE39625E1 (en) 2000-02-16 2007-05-15 Hallowell International, Llc Boosted air source heat pump
US20050044866A1 (en) * 2003-08-27 2005-03-03 Shaw David N. Boosted air source heat pump
US6931871B2 (en) 2003-08-27 2005-08-23 Shaw Engineering Associates, Llc Boosted air source heat pump
WO2006041682A1 (en) * 2004-10-06 2006-04-20 Hallowell International, Llc Oil balance system and method for compressors
US20060073026A1 (en) * 2004-10-06 2006-04-06 Shaw David N Oil balance system and method for compressors connected in series
US20080085195A1 (en) * 2004-10-06 2008-04-10 Hallowell International, Llc Oil balance system and method for compressors connected in series
US20080283133A1 (en) * 2004-10-06 2008-11-20 Hallowell International, Llc Oil balance system and method for compressors connected in series
US20090007588A1 (en) * 2004-10-06 2009-01-08 David Shaw Oil Balance System and Method for Compressors
US7651322B2 (en) * 2004-10-06 2010-01-26 Hallowell International, Llc Oil balance system and method for compressors connected in series
US7712329B2 (en) 2004-10-06 2010-05-11 David Shaw Oil balance system and method for compressors
US8075283B2 (en) * 2004-10-06 2011-12-13 Hallowell International, Llc Oil balance system and method for compressors connected in series
US20080173034A1 (en) * 2007-01-19 2008-07-24 Hallowell International, Llc Heat pump apparatus and method
US20140154105A1 (en) * 2012-12-03 2014-06-05 Danfoss (Tianjin) Ltd. Oil balancing apparatus and refrigeration device
US9657975B2 (en) * 2012-12-03 2017-05-23 Danfoss (Tianjin) Ltd. Oil balancing apparatus and refrigeration device
US11137180B1 (en) * 2020-04-30 2021-10-05 Trane Air Conditioning Systems (China) Co., Ltd. System and method for OCR control in paralleled compressors
US11649996B2 (en) 2020-04-30 2023-05-16 Trane Air Conditioning Systems (China) Co., Ltd. System and method for OCR control in paralleled compressors

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