FR2635824B1 - Turbomoteur a turbine a gaz entrainant par un reducteur des rotors a helices ou des rotors de soufflante - Google Patents

Turbomoteur a turbine a gaz entrainant par un reducteur des rotors a helices ou des rotors de soufflante

Info

Publication number
FR2635824B1
FR2635824B1 FR8911263A FR8911263A FR2635824B1 FR 2635824 B1 FR2635824 B1 FR 2635824B1 FR 8911263 A FR8911263 A FR 8911263A FR 8911263 A FR8911263 A FR 8911263A FR 2635824 B1 FR2635824 B1 FR 2635824B1
Authority
FR
France
Prior art keywords
rotors
gas turbine
reducer
propeller
driven
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 - Fee Related
Application number
FR8911263A
Other languages
English (en)
French (fr)
Other versions
FR2635824A1 (fr
Inventor
Klaus Rued
Rued Klaus
Alois Rohra
Rohra Alois
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.)
MTU Aero Engines AG
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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 MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Publication of FR2635824A1 publication Critical patent/FR2635824A1/fr
Application granted granted Critical
Publication of FR2635824B1 publication Critical patent/FR2635824B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02C7/12—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
    • 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
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047—Heating to prevent icing
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Supercharger (AREA)
  • Lubrication Of Internal Combustion Engines (AREA)
  • Motor Or Generator Cooling System (AREA)
FR8911263A 1988-08-25 1989-08-25 Turbomoteur a turbine a gaz entrainant par un reducteur des rotors a helices ou des rotors de soufflante Expired - Fee Related FR2635824B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3828834A DE3828834C1 (enExample) 1988-08-25 1988-08-25

Publications (2)

Publication Number Publication Date
FR2635824A1 FR2635824A1 (fr) 1990-03-02
FR2635824B1 true FR2635824B1 (fr) 1993-05-21

Family

ID=6361570

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8911263A Expired - Fee Related FR2635824B1 (fr) 1988-08-25 1989-08-25 Turbomoteur a turbine a gaz entrainant par un reducteur des rotors a helices ou des rotors de soufflante

Country Status (5)

Country Link
US (1) US4999994A (enExample)
JP (1) JP2790865B2 (enExample)
DE (1) DE3828834C1 (enExample)
FR (1) FR2635824B1 (enExample)
GB (1) GB2222855B (enExample)

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WO2006060004A1 (en) 2004-12-01 2006-06-08 United Technologies Corporation Combustor for turbine engine
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EP1828545A2 (en) 2004-12-01 2007-09-05 United Technologies Corporation Annular turbine ring rotor
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WO2006059993A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Tip turbine engine with multiple fan and turbine stages
EP1825116A2 (en) * 2004-12-01 2007-08-29 United Technologies Corporation Ejector cooling of outer case for tip turbine engine
DE602004019710D1 (de) 2004-12-01 2009-04-09 United Technologies Corp Fernbetätigung für eine verstellbare stufe eines verdichters für einen turbinenmotor
EP1825117B1 (en) 2004-12-01 2012-06-13 United Technologies Corporation Turbine engine with differential gear driven fan and compressor
WO2006110125A2 (en) * 2004-12-01 2006-10-19 United Technologies Corporation Stacked annular components for turbine engines
US9109537B2 (en) 2004-12-04 2015-08-18 United Technologies Corporation Tip turbine single plane mount
US20060130454A1 (en) * 2004-12-22 2006-06-22 Caterpillar Inc. Cooling system using gas turbine engine air stream
FR2902830B1 (fr) * 2006-06-27 2008-08-08 Airbus France Sas Turboreacteur pour aeronef
GB0708459D0 (en) * 2007-05-02 2007-06-06 Rolls Royce Plc A temperature controlling arrangement
US8967945B2 (en) 2007-05-22 2015-03-03 United Technologies Corporation Individual inlet guide vane control for tip turbine engine
US8708643B2 (en) * 2007-08-14 2014-04-29 General Electric Company Counter-rotatable fan gas turbine engine with axial flow positive displacement worm gas generator
US8210798B2 (en) * 2008-02-13 2012-07-03 United Technologies Corporation Cooled pusher propeller system
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FR2945270B1 (fr) * 2009-05-05 2011-04-22 Airbus France Dispositif de degivrage pour pales de propulseur de type propfan
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US20110182723A1 (en) * 2010-01-26 2011-07-28 Airbus Operations (S.A.S) Turbomachine aircraft propeller
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FR3023587B1 (fr) * 2014-07-10 2016-07-15 Turbomeca Turbomachine a systeme de refroidissement autonome d'equipements.
US10415475B2 (en) 2014-07-31 2019-09-17 Sikorsky Aircraft Corporation Gearbox oil cooling assembly
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US20160298543A1 (en) * 2015-04-13 2016-10-13 United Technologies Corporation Lubricant circulation system and method of circulating lubricant in a gas turbine engine
US9777595B2 (en) * 2015-05-05 2017-10-03 United Technologies Corporation Lubrication system for geared gas turbine engine
FR3041392A1 (fr) * 2015-09-17 2017-03-24 Labinal Power Systems Groupe de refroidissement pour un moteur ou une boite d'engrenages d'aeronef
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Also Published As

Publication number Publication date
GB2222855B (en) 1992-09-30
JP2790865B2 (ja) 1998-08-27
GB8919070D0 (en) 1989-10-04
JPH0281930A (ja) 1990-03-22
FR2635824A1 (fr) 1990-03-02
GB2222855A (en) 1990-03-21
US4999994A (en) 1991-03-19
DE3828834C1 (enExample) 1989-11-02

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Legal Events

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Effective date: 20060428