GB970207A - Cooling system for aircraft - Google Patents

Cooling system for aircraft

Info

Publication number
GB970207A
GB970207A GB47179/62A GB4717962A GB970207A GB 970207 A GB970207 A GB 970207A GB 47179/62 A GB47179/62 A GB 47179/62A GB 4717962 A GB4717962 A GB 4717962A GB 970207 A GB970207 A GB 970207A
Authority
GB
United Kingdom
Prior art keywords
heat exchanger
compressor
air
turbine
duct
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.)
Expired
Application number
GB47179/62A
Inventor
Bernard Exley Seed
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB47179/62A priority Critical patent/GB970207A/en
Publication of GB970207A publication Critical patent/GB970207A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • B64D13/08—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 the air being heated or cooled
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • 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
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Pulmonology (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

970,207. Refrigerating. ROLLS-ROYCE Ltd. Dec. 13, 1962, No. 47179/62. Heading F4H. [Also in Division F1] An aircraft cooling system receiving an airflow includes in series a compressor, a first heat exchanger having a passageway for the air flow coolant, a turbine driving the compressor and a second heat exchanger such that the airflow cools a fluid passing through, or in contact with, the second heat exchanger. A gas-turbine engine 5 having a compressor 8 supplies air through a duct 14 to an auxiliary compressor 16 driven by a turbine 18. Air leaving compressor 16 passes through a first heat exchanger 17 supplied with cooling ram air through a passage 6 and expands in a turbine 18 before passing into a second oil-cooling heat exchanger 19. Air from the oil cooler 19 exhausts into a duct 20 with an ejection effect.
GB47179/62A 1962-12-13 1962-12-13 Cooling system for aircraft Expired GB970207A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB47179/62A GB970207A (en) 1962-12-13 1962-12-13 Cooling system for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB47179/62A GB970207A (en) 1962-12-13 1962-12-13 Cooling system for aircraft

Publications (1)

Publication Number Publication Date
GB970207A true GB970207A (en) 1964-09-16

Family

ID=10444037

Family Applications (1)

Application Number Title Priority Date Filing Date
GB47179/62A Expired GB970207A (en) 1962-12-13 1962-12-13 Cooling system for aircraft

Country Status (1)

Country Link
GB (1) GB970207A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4782658A (en) * 1987-05-07 1988-11-08 Rolls-Royce Plc Deicing of a geared gas turbine engine
GB2251031A (en) * 1990-12-19 1992-06-24 Rolls Royce Plc Cooling air pick up for gas turbine engine
FR2905673A1 (en) * 2006-09-08 2008-03-14 Eurocopter France Air conditioner controlling method for rotocraft i.e. helicopter, involves monitoring lubricant i.e. oil, temperature and controlling capacity reduction of air conditioner of rotocraft when temperature attains/exceeds determined value
CN110645728A (en) * 2019-09-10 2020-01-03 北京星际荣耀空间科技有限公司 Refrigeration cycle system for aircraft and aircraft

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4782658A (en) * 1987-05-07 1988-11-08 Rolls-Royce Plc Deicing of a geared gas turbine engine
GB2204361A (en) * 1987-05-07 1988-11-09 Rolls Royce Plc Deicing of a geared gas turbine engine
GB2204361B (en) * 1987-05-07 1991-10-16 Rolls Royce Plc Deicing of a geared gas turbine.
GB2251031A (en) * 1990-12-19 1992-06-24 Rolls Royce Plc Cooling air pick up for gas turbine engine
GB2251031B (en) * 1990-12-19 1995-01-18 Rolls Royce Plc Cooling air pick up
FR2905673A1 (en) * 2006-09-08 2008-03-14 Eurocopter France Air conditioner controlling method for rotocraft i.e. helicopter, involves monitoring lubricant i.e. oil, temperature and controlling capacity reduction of air conditioner of rotocraft when temperature attains/exceeds determined value
CN110645728A (en) * 2019-09-10 2020-01-03 北京星际荣耀空间科技有限公司 Refrigeration cycle system for aircraft and aircraft

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