GB8330689D0 - Heat recovery system - Google Patents

Heat recovery system

Info

Publication number
GB8330689D0
GB8330689D0 GB838330689A GB8330689A GB8330689D0 GB 8330689 D0 GB8330689 D0 GB 8330689D0 GB 838330689 A GB838330689 A GB 838330689A GB 8330689 A GB8330689 A GB 8330689A GB 8330689 D0 GB8330689 D0 GB 8330689D0
Authority
GB
United Kingdom
Prior art keywords
heat recovery
recovery system
heat
recovery
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Withdrawn
Application number
GB838330689A
Other versions
GB2131094A (en
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of GB8330689D0 publication Critical patent/GB8330689D0/en
Publication of GB2131094A publication Critical patent/GB2131094A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • 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
    • F02C7/22—Fuel supply systems
    • F02C7/224—Heating fuel before feeding to the burner
    • 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
    • Y02T10/00—Road transport of goods or passengers
    • Y02T10/10—Internal combustion engine [ICE] based vehicles
    • Y02T10/12—Improving ICE efficiencies
    • 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)
  • Lubrication Of Internal Combustion Engines (AREA)
  • Other Air-Conditioning Systems (AREA)
  • Separation By Low-Temperature Treatments (AREA)
  • Waste-Gas Treatment And Other Accessory Devices For Furnaces (AREA)
GB08330689A 1982-11-29 1983-11-17 Engine oil heat recovery system Withdrawn GB2131094A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US44490582A 1982-11-29 1982-11-29

Publications (2)

Publication Number Publication Date
GB8330689D0 true GB8330689D0 (en) 1983-12-29
GB2131094A GB2131094A (en) 1984-06-13

Family

ID=23766828

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08330689A Withdrawn GB2131094A (en) 1982-11-29 1983-11-17 Engine oil heat recovery system

Country Status (5)

Country Link
JP (1) JPS59113240A (en)
DE (1) DE3342591A1 (en)
FR (1) FR2536842A1 (en)
GB (1) GB2131094A (en)
IT (1) IT8323794A0 (en)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4696156A (en) * 1986-06-03 1987-09-29 United Technologies Corporation Fuel and oil heat management system for a gas turbine engine
DE3714990A1 (en) * 1987-05-06 1988-12-01 Mtu Muenchen Gmbh PROPFAN TURBO ENGINE
GB8907788D0 (en) * 1989-04-06 1989-05-17 Rolls Royce Plc Management of heat generated by aircraft gas turbine installations
US5241814A (en) * 1989-04-06 1993-09-07 Rolls-Royce Plc Management of heat generated by aircraft gas turbine installations
US5177951A (en) * 1989-04-06 1993-01-12 Rolls-Royce Plc Method for management of heat generated by aircraft gas turbine installations
GB9027782D0 (en) * 1990-12-21 1991-02-13 Rolls Royce Plc Heat exchanger apparatus
US5826430A (en) * 1996-04-23 1998-10-27 Westinghouse Electric Corporation Fuel heating system used in conjunction with steam cooled combustors and transitions
US6584778B1 (en) * 2000-05-11 2003-07-01 General Electric Co. Methods and apparatus for supplying cooling air to turbine engines
US6415595B1 (en) 2000-08-22 2002-07-09 Hamilton Sundstrand Corporation Integrated thermal management and coolant system for an aircraft
FR2914365B1 (en) * 2007-03-28 2012-05-18 Airbus France SYSTEM FOR COOLING AND REGULATING EQUIPMENT TEMPERATURE OF A PROPELLANT AIRCRAFT ASSEMBLY.
US8438850B2 (en) * 2009-02-17 2013-05-14 General Electric Company Waste heat utilization for pre-heating fuel
GB201001410D0 (en) 2010-01-29 2010-03-17 Rolls Royce Plc Oil cooler
US9963994B2 (en) 2014-04-08 2018-05-08 General Electric Company Method and apparatus for clearance control utilizing fuel heating
AT515409B1 (en) * 2014-10-03 2015-09-15 Intellectual Capital And Asset Man Gmbh Method for utilizing the heat of aircraft jet engines and device for carrying out
FR3034464B1 (en) * 2015-04-03 2017-03-24 Snecma COOLING THE OIL CIRCUIT OF A TURBOMACHINE
US10260419B2 (en) 2015-07-31 2019-04-16 General Electric Company Cooling system
GB201811040D0 (en) 2018-07-05 2018-08-22 Rolls Royce Plc Cooling
FR3110938B1 (en) * 2020-05-28 2022-06-17 Safran Installation for heating cryogenic fuel
FR3133595A1 (en) * 2022-03-17 2023-09-22 Safran Helicopter Engines Device and method for regulating the temperature of a power source of an aircraft with a heat transfer fluid of a power transmission means

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR850267A (en) * 1939-12-12
GB720012A (en) * 1951-04-23 1954-12-08 Bristol Aeroplane Co Ltd Improvements in or relating to the cooling of aircraft propulsion plants
GB749684A (en) * 1952-12-12 1956-05-30 Rolls Royce Improvements in or relating to aircraft fuel systems
GB760243A (en) * 1953-11-06 1956-10-31 Rolls Royce Improvements in or relating to gas-turbine engines
GB912762A (en) * 1960-07-12 1962-12-12 Rolls Royce Heat exchange apparatus
US4041697A (en) * 1975-07-17 1977-08-16 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Oil cooling system for a gas turbine engine
US4404793A (en) * 1980-03-20 1983-09-20 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Apparatus for improving the fuel efficiency of a gas turbine engine
GB2095756B (en) * 1982-03-05 1985-01-16 United Technologies Corp Balancing the heat flow between components associated with a gas turbine engine

Also Published As

Publication number Publication date
FR2536842A1 (en) 1984-06-01
GB2131094A (en) 1984-06-13
IT8323794A0 (en) 1983-11-21
DE3342591A1 (en) 1984-05-30
JPS59113240A (en) 1984-06-29

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Legal Events

Date Code Title Description
732 Registration of transactions, instruments or events in the register (sect. 32/1977)
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)