DE2148755A1 - OElsystem fuer Turboluftstrahltriebwerke - Google Patents

OElsystem fuer Turboluftstrahltriebwerke

Info

Publication number
DE2148755A1
DE2148755A1 DE19712148755 DE2148755A DE2148755A1 DE 2148755 A1 DE2148755 A1 DE 2148755A1 DE 19712148755 DE19712148755 DE 19712148755 DE 2148755 A DE2148755 A DE 2148755A DE 2148755 A1 DE2148755 A1 DE 2148755A1
Authority
DE
Germany
Prior art keywords
oil
wall
oil tank
cooler
tank
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.)
Pending
Application number
DE19712148755
Other languages
German (de)
English (en)
Inventor
Geoffrey Beardsley
John Mcintyre
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.)
UK Secretary of State for Defence
Original Assignee
UK Secretary of State for Defence
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 UK Secretary of State for Defence filed Critical UK Secretary of State for Defence
Publication of DE2148755A1 publication Critical patent/DE2148755A1/de
Pending legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28D—HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT
    • F28D1/00—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators
    • F28D1/02—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid
    • F28D1/03—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with plate-like or laminated conduits
    • F28D1/0308—Heat-exchange apparatus having stationary conduit assemblies for one heat-exchange medium only, the media being in contact with different sides of the conduit wall, in which the other heat-exchange medium is a large body of fluid, e.g. domestic or motor car radiators with heat-exchange conduits immersed in the body of fluid with plate-like or laminated conduits the conduits being formed by paired plates touching each other
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/18—Lubricating arrangements
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28—HEAT EXCHANGE IN GENERAL
    • F28F—DETAILS OF HEAT-EXCHANGE AND HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION
    • F28F3/00—Plate-like or laminated elements; Assemblies of plate-like or laminated elements
    • F28F3/12—Elements constructed in the shape of a hollow panel, e.g. with channels
    • 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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
  • Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
DE19712148755 1970-10-02 1971-09-30 OElsystem fuer Turboluftstrahltriebwerke Pending DE2148755A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4692570 1970-10-02

Publications (1)

Publication Number Publication Date
DE2148755A1 true DE2148755A1 (de) 1972-07-20

Family

ID=10443089

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19712148755 Pending DE2148755A1 (de) 1970-10-02 1971-09-30 OElsystem fuer Turboluftstrahltriebwerke

Country Status (4)

Country Link
US (1) US3797561A (enExample)
DE (1) DE2148755A1 (enExample)
FR (1) FR2110172B1 (enExample)
GB (1) GB1322405A (enExample)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3447717A1 (de) * 1983-12-23 1985-07-04 United Technologies Corp., Hartford, Conn. Gasturbinenanlage
FR2614937A1 (fr) * 1987-05-06 1988-11-10 Mtu Muenchen Gmbh Turbopropulseur de type propfan a systeme de lubrification d'huile annulaire
DE3828834C1 (enExample) * 1988-08-25 1989-11-02 Mtu Muenchen Gmbh

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4002224A (en) * 1975-02-26 1977-01-11 Westinghouse Electric Corporation Turbine lubrication and emergency gas system
US4151710A (en) * 1977-03-11 1979-05-01 United Technologies Corporation Lubrication cooling system for aircraft engine accessory
US4254618A (en) * 1977-08-18 1981-03-10 General Electric Company Cooling air cooler for a gas turbofan engine
US4187675A (en) * 1977-10-14 1980-02-12 The United States Of America As Represented By The Secretary Of The Air Force Compact air-to-air heat exchanger for jet engine application
US7377098B2 (en) 2004-08-26 2008-05-27 United Technologies Corporation Gas turbine engine frame with an integral fluid reservoir and air/fluid heat exchanger
US7377100B2 (en) * 2004-08-27 2008-05-27 Pratt & Whitney Canada Corp. Bypass duct fluid cooler
US8205426B2 (en) * 2006-07-31 2012-06-26 General Electric Company Method and apparatus for operating gas turbine engines
US7862293B2 (en) * 2007-05-03 2011-01-04 Pratt & Whitney Canada Corp. Low profile bleed air cooler
US8763363B2 (en) * 2007-07-06 2014-07-01 General Electric Company Method and system for cooling fluid in a turbine engine
US9957918B2 (en) 2007-08-28 2018-05-01 United Technologies Corporation Gas turbine engine front architecture
EP2075194B1 (fr) 2007-12-27 2017-08-16 Techspace Aero Echangeur de chaleur air-huile pour turboréacteur, turboréacteur associé et utilisation dudit échangeur
US8181443B2 (en) * 2008-12-10 2012-05-22 Pratt & Whitney Canada Corp. Heat exchanger to cool turbine air cooling flow
US8627667B2 (en) * 2008-12-29 2014-01-14 Roll-Royce Corporation Gas turbine engine duct having a coupled fluid volume
US8544531B2 (en) * 2010-06-11 2013-10-01 Hs Marston Aerospace Ltd. Surface cooler with noise reduction
US8973552B2 (en) * 2011-06-27 2015-03-10 United Technologies Corporation Integral oil system
US9194294B2 (en) 2012-05-07 2015-11-24 United Technologies Corporation Gas turbine engine oil tank
US9945252B2 (en) 2012-07-05 2018-04-17 United Technologies Corporation Gas turbine engine oil tank with integrated packaging configuration
WO2014134040A1 (en) 2013-02-28 2014-09-04 United Technologies Corporation Integrated thermal management with nacelle laminar flow control for geared architecture gas turbine engine
EP2971672B1 (en) * 2013-03-15 2018-09-26 United Technologies Corporation Gas turbine engine with air-oil cooler oil tank
US10578020B2 (en) 2015-07-21 2020-03-03 Unison Industries, Llc Integral oil tank heat exchanger
US10570824B2 (en) * 2015-11-23 2020-02-25 United Technologies Corporation Near zero velocity lubrication system for a turbine engine
EP3181833B1 (en) * 2015-12-17 2022-09-07 Rolls-Royce Deutschland Ltd & Co KG Heat exchange system for a power gear box, a power gear box and a turbo engine with a power gear box
EP3181834B1 (en) * 2015-12-17 2022-09-07 Rolls-Royce Deutschland Ltd & Co KG Heat exchange system for a power gear box, a power gear box and a turbo engine with a power gear box
FR3046199B1 (fr) * 2015-12-23 2017-12-29 Snecma Turbomachine comprenant un echangeur air-huile surfacique integre a un compartiment inter-veines
US10823061B2 (en) * 2016-07-15 2020-11-03 General Electric Company Engine air inlet having a double-panel heated wall
US10816007B2 (en) * 2016-11-11 2020-10-27 Pratt & Whitney Canada Corp. Oil tank installation in gas turbine engine
FR3065490B1 (fr) * 2017-04-24 2019-07-12 Safran Aircraft Engines Ensemble propulsif pour aeronef comportant des echangeurs de chaleur air-liquide
BE1025642B1 (fr) * 2017-10-16 2019-05-15 Safran Aero Boosters S.A. Carter de compresseur avec reservoir d'huile pour turbomachine
FR3086325B1 (fr) * 2018-09-24 2020-11-20 Safran Aircraft Engines Reservoir auxiliaire d'huile pour une turbomachine d'aeronef
GB2589125B (en) 2019-11-21 2022-10-19 Gkn Aerospace Sweden Ab Heat exchanger integration
US20210262388A1 (en) 2020-02-20 2021-08-26 Pratt & Whitney Canada Corp. Integrated oil tank with passive thermal modulation
US12510002B2 (en) * 2023-07-12 2025-12-30 General Electric Company Lubrication system for a turbine engine

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2428280A (en) * 1944-08-05 1947-09-30 Garrett Corp Control device for oil coolers
US2830798A (en) * 1953-02-13 1958-04-15 Garrett Corp Axial flow oil cooler having cross baffles

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3447717A1 (de) * 1983-12-23 1985-07-04 United Technologies Corp., Hartford, Conn. Gasturbinenanlage
DE3447717C2 (de) * 1983-12-23 1998-02-12 United Technologies Corp Axial durchströmtes Bläsertriebwerk
FR2614937A1 (fr) * 1987-05-06 1988-11-10 Mtu Muenchen Gmbh Turbopropulseur de type propfan a systeme de lubrification d'huile annulaire
DE3828834C1 (enExample) * 1988-08-25 1989-11-02 Mtu Muenchen Gmbh

Also Published As

Publication number Publication date
FR2110172A1 (enExample) 1972-06-02
FR2110172B1 (enExample) 1977-08-05
GB1322405A (en) 1973-07-04
US3797561A (en) 1974-03-19

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