GB2195174A - Miniaturized high frequency electrically driven vapor cycle refrigeration system - Google Patents
Miniaturized high frequency electrically driven vapor cycle refrigeration system Download PDFInfo
- Publication number
- GB2195174A GB2195174A GB08719539A GB8719539A GB2195174A GB 2195174 A GB2195174 A GB 2195174A GB 08719539 A GB08719539 A GB 08719539A GB 8719539 A GB8719539 A GB 8719539A GB 2195174 A GB2195174 A GB 2195174A
- Authority
- GB
- United Kingdom
- Prior art keywords
- compressor
- refrigeration system
- high frequency
- evaporator
- inlet
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
- 238000005057 refrigeration Methods 0.000 title claims description 10
- 239000012530 fluid Substances 0.000 claims description 12
- 239000003507 refrigerant Substances 0.000 claims description 9
- 230000006698 induction Effects 0.000 claims description 6
- 239000012071 phase Substances 0.000 description 4
- 239000011555 saturated liquid Substances 0.000 description 4
- 229920006395 saturated elastomer Polymers 0.000 description 3
- 239000012080 ambient air Substances 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 230000003245 working effect Effects 0.000 description 2
- AJDIZQLSFPQPEY-UHFFFAOYSA-N 1,1,2-Trichlorotrifluoroethane Chemical compound FC(F)(Cl)C(F)(Cl)Cl AJDIZQLSFPQPEY-UHFFFAOYSA-N 0.000 description 1
- 241000282326 Felis catus Species 0.000 description 1
- 238000009835 boiling Methods 0.000 description 1
- 238000009833 condensation Methods 0.000 description 1
- 230000005494 condensation Effects 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 238000007710 freezing Methods 0.000 description 1
- 230000008014 freezing Effects 0.000 description 1
- 239000007791 liquid phase Substances 0.000 description 1
- 239000000314 lubricant Substances 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000009834 vaporization Methods 0.000 description 1
- 230000008016 vaporization Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60H—ARRANGEMENTS OF HEATING, COOLING, VENTILATING OR OTHER AIR-TREATING DEVICES SPECIALLY ADAPTED FOR PASSENGER OR GOODS SPACES OF VEHICLES
- B60H1/00—Heating, cooling or ventilating [HVAC] devices
- B60H1/00357—Air-conditioning arrangements specially adapted for particular vehicles
- B60H1/00414—Air-conditioning arrangements specially adapted for particular vehicles for military, emergency, safety or security vehicles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60H—ARRANGEMENTS OF HEATING, COOLING, VENTILATING OR OTHER AIR-TREATING DEVICES SPECIALLY ADAPTED FOR PASSENGER OR GOODS SPACES OF VEHICLES
- B60H1/00—Heating, cooling or ventilating [HVAC] devices
- B60H1/32—Cooling devices
- B60H1/3204—Cooling devices using compression
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
-
- 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
- F25B1/04—Compression machines, plants or systems with non-reversible cycle with compressor of rotary type
-
- 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
- F25B41/00—Fluid-circulation arrangements
- F25B41/20—Disposition of valves, e.g. of on-off valves or flow control valves
-
- 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
- F25B47/00—Arrangements for preventing or removing deposits or corrosion, not provided for in another subclass
- F25B47/006—Arrangements for preventing or removing deposits or corrosion, not provided for in another subclass for preventing frost
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
- B64D2013/0603—Environmental Control Systems
- B64D2013/0644—Environmental Control Systems including electric motors or generators
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/06—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being conditioned
- B64D2013/0603—Environmental Control Systems
- B64D2013/0674—Environmental Control Systems comprising liquid subsystems
-
- 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
- F25B2400/00—General 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
- F25B2400/04—Refrigeration circuit bypassing means
- F25B2400/0403—Refrigeration circuit bypassing means for the condenser
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/50—On board measures aiming to increase energy efficiency
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- Thermal Sciences (AREA)
- General Engineering & Computer Science (AREA)
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Pulmonology (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
1 GB2195174A 1
SPECIFICATION
Miniaturized high frequency electrically driven vapor cycle refrigeration system BACKGROUND OF THE INVENTION
Conventional D.C. or low frequency A.C. electric motors have weight and volume characteristics that cannot be tolerated in certain military and automotive applications which require that component size be minimized. Such miniaturized systems are particularly desirable for combat vehicle and aircraft applications.
SUMMARY OF THE INVENTION 80
The. refrigeration system of the present in vention utilizes a small high speed centrifugal compressor driven by a directly coupled, high frequency, three phase, induction motor. A feature of the system comprises a hot gas bypass line that extends from the compressor outlet to the inlet side of the evaporator whereby hot gas flows directly from the com pressor to the evaporator for the purpose of maintaining relatively constant compressor 90 flow over a range of conditions.
The refrigeration subsystem is a reverse Rankine vapor cycle, operating primarily within the two-phase (liquid-vapor) of the Rl 13 working fluid. In the refrigeration subsystem, working fluid leaves the receiver as a high pressure, saturated liquid and passes through a dryer unit before entering the expansion valve. The expansion valve throttles the work ing fluid to the evaporator pressure. As a re sult, the fluid entering the evaporator is in a two-phase condition. In the evaporator, the liquid phase is vaporized at constant pressure and temperature, and the latent heat of vapor ization cools the incoming ambient air. The saturated vapor which leaves the evaporator is then compressed to condenser pressure by the refrigerant compressor. The fluid leaving the compressor is a slightly superheated va por. The working fluid is then condensed at constant pressure to the saturated liquid con dition in the condenser using ambient air to remove the heat of condensation. The cycle is then completed as saturated liquid from the condenser enters the receiver/reservoir. This cycle absorbs heat at low temperature in the evaporator and rejects this heat plus the refri gerant compressor power at high temperature in the condenser.
The high frequency refrigerant compressor 120 induction motor is driven either directly from a high speed permanent magnet alternator or from an appropriate inverter.
R1 13 was selected as the refrigerant work- ing fluid for the vapor cycle because of its special suitability for use with centrifugal compressors. The relatively high specific volume of R1 13 permits acceptable compressor rotational speeds and reasonable aerodynamic and mechanical design criteria.
BRIEF DESCRIPTION OF THE DRAWING
The drawing is a schematic of a reverse Rankine vapor compressionrefrigeration sys- tem in accordance with the present invention.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENT OF THE INVENTION
As seen in the drawing, a refrigeration systern 10, in accordance with a constructed embodiment of the instant invention, comprises a high-speed, high-frequency, three phase, brushless, A.C. electric induction motor 12, capable of driving a directly coupled two-stage centrifugal compressor 14 at, for example, 112,000 RPM. The compressor 14 utilizes a centrifugal impeller operating at a design pressure ratio of 5.4:1. The impeller embodies an eight-splitter/vane, 50 degree lean-back confi- guration operating at an actual 111,375 RPM.
In, for example, a combat vehicle environmental protection system application, a sixpole power subsystem turboalternator 15 may be utilized having an output frequency of 3750 Hz. The alterntor 15 is rotated at 75, 000 RPM, a 6:4 pole ratio establishing a nominal motor speed of 112,500 RPM and, therefore, a nominal compressor rotor speed of 112,500 revolutions per minute.
The direct A.C. motor drive makes it possible to eliminate the shaft seal common with belt driven compressors, and to assemble the unit as a hermetically sealed assembly. Combination of the high speed/high frequency induc- tion motor, having a minimum speed of 70,000 RPM, powering the centrifugal compressor results in an overall package that is smaller and lighter than comparable low speed piston or vane-type systems. Analysis indi- cates system volume and weight savings in the 30% to 50% range.
The refrigerant selected for the system 10 is Freon R1 13 due to its suitability for use with centrifugal compressors. When compared to comparable refrigerant fluorocarbons the higher specific volume characteristics of Freon R1 13 results in reasonable acrodynamic and mechanical design criteria. Although Freon R1 13 exhibits a relatively high freezing point, its boiling point is elevated as well meaning that it can be shipped in unpressurized containers. A relatively low density in the solid state, as opposed to the liquid state, acts to prevent damage to the refrigeration system evaporator in the event of a freeze-up.
In accordance with one feature of the instant invention, a bypass valve 16 is disposed in a line 17 that forms a first fluid flow circuit from the compressor 14 to an evaporator 18.
The hot gas bypass valve 16 controls flow of hot gas from the compressor outlet directly to the evaporator 18 whereby a small amount of superheated vapor acts to maintain constant compressor flow over a range of conditions and eliminates evaporator icing.
2 GB2195174A 2 A second parallel fluid flow path from the compressor 14 to the evaporator 18 comprises a line 19 having a condenser 20, Freon R1 13 reservoir 22, filter 24 and expansion valve 26 therein. In operation, saturated vapor is compressed isentropically to a superheated vapor by the motor driven compressor 14. As the Freon 113 passes through the compressor 14, oil may be added to aid in the lubrication thereof. The oil is separated out in the compressor diffuser stage and circulated back to the compressor inlet preventing residual lubricant in the remainder of the system. Superheated vapor from the compressor 14 flows through both the first flow path comprising the line 17 and valve 16 and through the second flow path, comprising the line 19 to the condenser 20 which acts to remove heat at constant pressure, turning the vapor into a saturated liquid. As a liquid, the refrigerant flows to the expansion valve 26 with minimum loss of enthalpy. Thereafter, the refrigerant passes at constant pressure through the evaporator 18. Ambient heat entering the evaporator 18 vaporizes the working fluid into the saturated vapor state, for return to the compressor 14 thus, completing the cycle. While the preferred embodiment of the in- vention has been disclosed, it should be appreciated that the- invention is susceptible of modification without departing from the scope of the following claims.
Claims (3)
1. A miniaturized refrigeration system com prising:
a source of high frequency alternating cur rent, a high speed high frequency induction mo tor, a centrifugal refrigerant compressor directly coupled to said motor, an evaporator having an outlet connected to an inlet on said compressor, a first fluid flow path from an outlet on said compressor to an inlet of said evaporator having a valve therein for controlling the flow of superheated vapor from said com pressor to said eyaporator thereby to main tain relatively constant compressor flow over a relatively wide range of conditions, and a second fluid flow path from the outlet on said compressor to the inlet of said evapo rator comprising a condenser and an expan sion valve.
2. A refrigeration system in accordance with claim 1 wherein the operating speed of said induction motor and compressor is over 70,000 revolutions per minute.
3. A refrigeration system constructed and arranged to operate substantially as hereinbefore described with reference to and as illustrated in the accompanying drawings.
Published 1988atThe Patent Office, State House, 66/71 High Holborn, London WC 1 R 4TP. Further copies may be obtained from The Patent Office, Sales Branch, St Mary Cray, Orpington, Kent BR5 3RD. Printed by Burgess & Son (Abingdon) Ltd. Con. 1/87.
1 1 i
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US90693386A | 1986-09-15 | 1986-09-15 |
Publications (2)
Publication Number | Publication Date |
---|---|
GB8719539D0 GB8719539D0 (en) | 1987-09-23 |
GB2195174A true GB2195174A (en) | 1988-03-30 |
Family
ID=25423247
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB08719539A Withdrawn GB2195174A (en) | 1986-09-15 | 1987-08-19 | Miniaturized high frequency electrically driven vapor cycle refrigeration system |
Country Status (3)
Country | Link |
---|---|
JP (1) | JPS6375446A (en) |
DE (1) | DE3728518A1 (en) |
GB (1) | GB2195174A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2564147A (en) * | 2017-07-05 | 2019-01-09 | Microcold Ltd | Turbine based heat transfer system |
CN109900002A (en) * | 2017-12-07 | 2019-06-18 | 盾安美斯泰克股份有限公司 | Heating, ventilation, air-conditioning and the refrigeration system of ability are stabilized with mass flow |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE29901789U1 (en) | 1999-02-02 | 1999-04-01 | Rußland, Wolfgang, 82216 Germerswang | Power heater |
JP4605871B2 (en) * | 2000-08-25 | 2011-01-05 | 富士通セミコンダクター株式会社 | Microprocessor |
WO2019060752A1 (en) * | 2017-09-25 | 2019-03-28 | Johnson Controls Technology Company | Two step oil motive eductor system |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2149900A (en) * | 1983-10-19 | 1985-06-19 | Ferguson Seacabs Limited | Refrigeration apparatus |
US4546618A (en) * | 1984-09-20 | 1985-10-15 | Borg-Warner Corporation | Capacity control systems for inverter-driven centrifugal compressor based water chillers |
-
1987
- 1987-08-19 GB GB08719539A patent/GB2195174A/en not_active Withdrawn
- 1987-08-26 DE DE19873728518 patent/DE3728518A1/en not_active Withdrawn
- 1987-09-14 JP JP62230892A patent/JPS6375446A/en active Pending
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2149900A (en) * | 1983-10-19 | 1985-06-19 | Ferguson Seacabs Limited | Refrigeration apparatus |
US4546618A (en) * | 1984-09-20 | 1985-10-15 | Borg-Warner Corporation | Capacity control systems for inverter-driven centrifugal compressor based water chillers |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2564147A (en) * | 2017-07-05 | 2019-01-09 | Microcold Ltd | Turbine based heat transfer system |
CN109900002A (en) * | 2017-12-07 | 2019-06-18 | 盾安美斯泰克股份有限公司 | Heating, ventilation, air-conditioning and the refrigeration system of ability are stabilized with mass flow |
Also Published As
Publication number | Publication date |
---|---|
GB8719539D0 (en) | 1987-09-23 |
JPS6375446A (en) | 1988-04-05 |
DE3728518A1 (en) | 1988-03-24 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |