FR933000A - Perfectionnements aux, ou concernant les turbines à combustion interne, pour la propulsion aérienne - Google Patents

Perfectionnements aux, ou concernant les turbines à combustion interne, pour la propulsion aérienne

Info

Publication number
FR933000A
FR933000A FR933000DA FR933000A FR 933000 A FR933000 A FR 933000A FR 933000D A FR933000D A FR 933000DA FR 933000 A FR933000 A FR 933000A
Authority
FR
France
Prior art keywords
relating
internal combustion
air propulsion
combustion turbines
turbines
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
Other languages
English (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.)
Metropolitan Vickers Electrical Co Ltd
Original Assignee
Metropolitan Vickers Electrical Co Ltd
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 Metropolitan Vickers Electrical Co Ltd filed Critical Metropolitan Vickers Electrical Co Ltd
Application granted granted Critical
Publication of FR933000A publication Critical patent/FR933000A/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/072—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with counter-rotating, e.g. fan rotors
    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • F02C3/067—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages having counter-rotating rotors
    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • F02C3/073—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages the compressor and turbine stages being concentric
    • 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)
FR933000D 1941-10-14 1946-08-28 Perfectionnements aux, ou concernant les turbines à combustion interne, pour la propulsion aérienne Expired FR933000A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB933000X 1941-10-14

Publications (1)

Publication Number Publication Date
FR933000A true FR933000A (fr) 1948-04-07

Family

ID=10747491

Family Applications (1)

Application Number Title Priority Date Filing Date
FR933000D Expired FR933000A (fr) 1941-10-14 1946-08-28 Perfectionnements aux, ou concernant les turbines à combustion interne, pour la propulsion aérienne

Country Status (1)

Country Link
FR (1) FR933000A (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0244515A3 (fr) * 1986-04-16 1989-04-12 The Boeing Company Moteur d'avion à soufflante avec carénage tournant
WO2004074638A1 (fr) * 2003-02-19 2004-09-02 Mtu Aero Engines Gmbh Dispositif destine a influencer la transition thermique dans des appareils rotatifs, notamment des turbines a gaz
EP2415965A3 (fr) * 2010-08-02 2013-05-01 Rolls-Royce plc Moteur à turbine à gaz

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0244515A3 (fr) * 1986-04-16 1989-04-12 The Boeing Company Moteur d'avion à soufflante avec carénage tournant
WO2004074638A1 (fr) * 2003-02-19 2004-09-02 Mtu Aero Engines Gmbh Dispositif destine a influencer la transition thermique dans des appareils rotatifs, notamment des turbines a gaz
US7422416B2 (en) 2003-02-19 2008-09-09 Mtu Aero Engines Gmbh Device for effecting heat transfer to rotating equipment, in particular gas turbines
EP2415965A3 (fr) * 2010-08-02 2013-05-01 Rolls-Royce plc Moteur à turbine à gaz

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