DE69105146D1 - Integriertes triebwerk mit mehrfachfunktion und kraftübertragungsgerät dafür. - Google Patents
Integriertes triebwerk mit mehrfachfunktion und kraftübertragungsgerät dafür.Info
- Publication number
- DE69105146D1 DE69105146D1 DE69105146T DE69105146T DE69105146D1 DE 69105146 D1 DE69105146 D1 DE 69105146D1 DE 69105146 T DE69105146 T DE 69105146T DE 69105146 T DE69105146 T DE 69105146T DE 69105146 D1 DE69105146 D1 DE 69105146D1
- Authority
- DE
- Germany
- Prior art keywords
- power transmission
- transmission device
- multiple function
- integrated engine
- engine
- 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 - Lifetime
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
- F02C7/32—Arrangement, mounting, or driving, of auxiliaries
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D41/00—Power installations for auxiliary purposes
-
- 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
- F02C7/26—Starting; Ignition
- F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
- F02C7/275—Mechanical drives
- F02C7/277—Mechanical drives the starter being a separate turbine
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2220/00—Application
- F05D2220/50—Application for auxiliary power units (APU's)
-
- 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
- Y02T50/40—Weight reduction
-
- 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
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S74/00—Machine element or mechanism
- Y10S74/05—Gas turbine with gearing
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T74/00—Machine element or mechanism
- Y10T74/19—Gearing
- Y10T74/19023—Plural power paths to and/or from gearing
- Y10T74/19051—Single driven plural drives
- Y10T74/1907—Parallel and aligned
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/587,709 US5201798A (en) | 1990-09-24 | 1990-09-24 | Multifunction integrated power unit and power transfer apparatus therefor |
PCT/US1991/006344 WO1992005351A1 (en) | 1990-09-24 | 1991-09-05 | Multifunction integrated power unit and power transfer apparatus therefor |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69105146D1 true DE69105146D1 (de) | 1994-12-15 |
DE69105146T2 DE69105146T2 (de) | 1995-04-13 |
Family
ID=24350881
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69105146T Expired - Lifetime DE69105146T2 (de) | 1990-09-24 | 1991-09-05 | Integriertes triebwerk mit mehrfachfunktion und kraftübertragungsgerät dafür. |
Country Status (4)
Country | Link |
---|---|
US (1) | US5201798A (de) |
EP (1) | EP0550658B1 (de) |
DE (1) | DE69105146T2 (de) |
WO (1) | WO1992005351A1 (de) |
Families Citing this family (52)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5343778A (en) * | 1992-11-09 | 1994-09-06 | Alliedsignal Inc. | Multifunction secondary power system |
US6732529B2 (en) | 2001-11-16 | 2004-05-11 | Pratt & Whitney Canada Corp. | Off loading clutch for gas turbine engine starting |
US6829899B2 (en) | 2002-01-25 | 2004-12-14 | Honeywell International Inc. | Jet fuel and air system for starting auxiliary power unit |
US6860726B2 (en) | 2002-02-05 | 2005-03-01 | The Boeing Company | Dual drive for hydraulic pump and air boost compressor |
US6942451B1 (en) | 2003-06-03 | 2005-09-13 | Hamilton Sundstrand Corporation | Damping system for an expendable gas turbine engine |
US7194866B1 (en) | 2003-06-20 | 2007-03-27 | Hamilton Sundstrand Corporation | Static structure for an expendable gas turbine engine |
US8438858B1 (en) | 2003-08-20 | 2013-05-14 | Hamilton Sundstrand Corporation | Rotational system for an expendable gas turbine engine |
GB0416344D0 (en) * | 2004-07-22 | 2004-08-25 | Rolls Royce Plc | Generator assembly |
US7922117B2 (en) * | 2004-08-30 | 2011-04-12 | Hamilton Sundstrand Corporation | Primary panel and motor controller integration for aircraft power distribution system |
US7930953B2 (en) * | 2006-11-30 | 2011-04-26 | Honeywell International Inc. | Gearbox with removable oil tank |
US7937949B2 (en) * | 2007-07-02 | 2011-05-10 | Honeywell International, Inc. | Emergency power engine restart system |
US8113317B2 (en) * | 2007-07-06 | 2012-02-14 | Honeywell International Inc. | Electric motor driven lubrication pump control system and method that accomodates turbomachine windmill operation |
FR2928696B1 (fr) * | 2008-03-14 | 2013-09-27 | Hispano Suiza Sa | Assemblage pour l'entrainement d'accessoires d'une turbine a gaz |
EP2123884B1 (de) * | 2008-05-13 | 2015-03-04 | Rolls-Royce Corporation | Doppelkupplungseinheit |
ES2363897B1 (es) | 2008-10-24 | 2012-07-04 | Airbus Operations, S.L. | Unidad de potencia auxiliar (apu) de una aeronave |
CN102198860B (zh) * | 2010-03-24 | 2016-02-03 | 哈米尔顿森德斯特兰德公司 | 混合式冲压空气涡轮 |
FR2975547B1 (fr) * | 2011-05-20 | 2013-06-07 | Turbomeca | Procede de rationalisation de chaine de composants electriques d'un aeronef, architecture de mise en oeuvre et aeronef correspondant |
FR2981986B1 (fr) * | 2011-10-26 | 2016-03-04 | Snecma | Boitier d'entrainement d'accessoires pour turboreacteur |
ITFI20110247A1 (it) * | 2011-11-14 | 2013-05-15 | Nuovo Pignone Spa | "device and method for slow turning of an aeroderivative gas turbine" |
FR3012422B1 (fr) * | 2013-10-31 | 2016-12-09 | Microturbo | Procede et systeme de generation de puissance auxiliaire dans un aeronef |
FR3024180B1 (fr) * | 2014-07-28 | 2016-07-22 | Turbomeca | Dispositif pneumatique de reactivation rapide d'un turbomoteur, architecture d'un systeme propulsif d'un helicoptere multi-moteur equipe d'un tel dispositif et helicoptere correspondant |
JP6343243B2 (ja) * | 2015-03-09 | 2018-06-13 | 川崎重工業株式会社 | 航空機用発電装置 |
US10040577B2 (en) | 2016-02-12 | 2018-08-07 | United Technologies Corporation | Modified start sequence of a gas turbine engine |
US10436064B2 (en) | 2016-02-12 | 2019-10-08 | United Technologies Corporation | Bowed rotor start response damping system |
US10539079B2 (en) | 2016-02-12 | 2020-01-21 | United Technologies Corporation | Bowed rotor start mitigation in a gas turbine engine using aircraft-derived parameters |
US9664070B1 (en) | 2016-02-12 | 2017-05-30 | United Technologies Corporation | Bowed rotor prevention system |
US10174678B2 (en) | 2016-02-12 | 2019-01-08 | United Technologies Corporation | Bowed rotor start using direct temperature measurement |
US10443505B2 (en) | 2016-02-12 | 2019-10-15 | United Technologies Corporation | Bowed rotor start mitigation in a gas turbine engine |
US10508567B2 (en) | 2016-02-12 | 2019-12-17 | United Technologies Corporation | Auxiliary drive bowed rotor prevention system for a gas turbine engine through an engine accessory |
US10125691B2 (en) | 2016-02-12 | 2018-11-13 | United Technologies Corporation | Bowed rotor start using a variable position starter valve |
US10443507B2 (en) | 2016-02-12 | 2019-10-15 | United Technologies Corporation | Gas turbine engine bowed rotor avoidance system |
US10125636B2 (en) | 2016-02-12 | 2018-11-13 | United Technologies Corporation | Bowed rotor prevention system using waste heat |
US10508601B2 (en) | 2016-02-12 | 2019-12-17 | United Technologies Corporation | Auxiliary drive bowed rotor prevention system for a gas turbine engine |
US10598047B2 (en) | 2016-02-29 | 2020-03-24 | United Technologies Corporation | Low-power bowed rotor prevention system |
US10717539B2 (en) * | 2016-05-05 | 2020-07-21 | Pratt & Whitney Canada Corp. | Hybrid gas-electric turbine engine |
US10787933B2 (en) | 2016-06-20 | 2020-09-29 | Raytheon Technologies Corporation | Low-power bowed rotor prevention and monitoring system |
US10358936B2 (en) | 2016-07-05 | 2019-07-23 | United Technologies Corporation | Bowed rotor sensor system |
US10221774B2 (en) | 2016-07-21 | 2019-03-05 | United Technologies Corporation | Speed control during motoring of a gas turbine engine |
EP3273006B1 (de) | 2016-07-21 | 2019-07-03 | United Technologies Corporation | Verwendung eines alternierenden anlassers während des anfahrens mit mehreren motoren |
EP3273016B1 (de) | 2016-07-21 | 2020-04-01 | United Technologies Corporation | Koordination während des anlassens eines gasturbinenmotors |
US10618666B2 (en) | 2016-07-21 | 2020-04-14 | United Technologies Corporation | Pre-start motoring synchronization for multiple engines |
US10384791B2 (en) | 2016-07-21 | 2019-08-20 | United Technologies Corporation | Cross engine coordination during gas turbine engine motoring |
US20180030900A1 (en) * | 2016-08-01 | 2018-02-01 | Honeywell International Inc. | Air Turbine Starter with Integrated Motor for Main Engine Cooling |
US10787968B2 (en) | 2016-09-30 | 2020-09-29 | Raytheon Technologies Corporation | Gas turbine engine motoring with starter air valve manual override |
US10443543B2 (en) | 2016-11-04 | 2019-10-15 | United Technologies Corporation | High compressor build clearance reduction |
US10823079B2 (en) | 2016-11-29 | 2020-11-03 | Raytheon Technologies Corporation | Metered orifice for motoring of a gas turbine engine |
US10843804B2 (en) * | 2017-08-01 | 2020-11-24 | Honeywell International Inc. | Cabin outflow air energy optimized cabin pressurizing system |
RU2670997C1 (ru) * | 2018-06-01 | 2018-10-29 | Акционерное общество "РЭП Холдинг" (АО "РЭПХ") | Пусковая система газотурбинного двигателя |
US11015532B2 (en) | 2018-10-18 | 2021-05-25 | Rolls-Royce North American Technologies, Inc. | Parallel starter/generator and air turbine starter |
US11261795B2 (en) | 2018-10-18 | 2022-03-01 | Rolls-Royce North American Technologies, Inc. | Dual mode starter generator |
US20230076951A1 (en) * | 2021-09-08 | 2023-03-09 | Rolls-Royce North American Technologies Inc. | Electrically driven redundant fuel and oil pumping system for gas turbine engines |
US20230072590A1 (en) * | 2021-09-08 | 2023-03-09 | Rolls-Royce North American Technologies Inc. | Redundant electrically driven fuel and oil pumping system for gas turbines |
Family Cites Families (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1479993A (en) * | 1918-09-16 | 1924-01-08 | Curtiss Aeroplane & Motor Co | Motive-power system for aircraft |
US1886327A (en) * | 1932-03-14 | 1932-11-01 | Carlson Edward | Safety motor for aircraft |
US2119156A (en) * | 1936-11-13 | 1938-05-31 | Eclipse Aviat Corp | Power plant |
FR868516A (fr) * | 1940-01-02 | 1942-01-05 | Daimler Benz Ag | Commande d'appareils auxiliaires pour moteurs d'avions |
US2611239A (en) * | 1949-03-18 | 1952-09-23 | Avco Mfg Corp | Fuel and combustion supporting medium control for turbine engine starters using excess fuel for cooling |
US2643511A (en) * | 1949-10-07 | 1953-06-30 | Avco Mfg Corp | Engine starter having combustion chamber supplied with fuel and combustion supporting medium for constant ratio by weight |
GB703262A (en) * | 1950-10-16 | 1954-02-03 | Rolls Royce | Improvements in or relating to gas-turbine engines |
US2777301A (en) * | 1952-06-30 | 1957-01-15 | Garrett Corp | All-purpose power and air conditioning system |
FR1280193A (fr) * | 1961-01-06 | 1961-12-29 | United Aircraft Corp | Système de démarrage pour moteurs |
GB1103417A (en) * | 1965-12-07 | 1968-02-14 | Dowty Rotol Ltd | Engine installations and starting means therefor |
US3514945A (en) * | 1968-10-04 | 1970-06-02 | Avco Corp | Gas turbine accessory power drive unit |
US3662975A (en) * | 1970-09-21 | 1972-05-16 | Robert E Driskill | Auxiliary electrical generating system for jet aircraft |
US3965673A (en) * | 1973-05-19 | 1976-06-29 | Vereinigte Flugtechnische Werke-Fokker Gesellschaft Mit Beschrankter Haftung | Apparatus for starting aircraft engines and for operating auxiliary on-board power generating equipment |
US3967132A (en) * | 1974-11-26 | 1976-06-29 | Takamine Bruce N | Air operated power transfer apparatus |
DE2519152C2 (de) * | 1975-04-30 | 1982-11-25 | Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen | Vorrichtung zum Anlassen von Flugzeugtriebwerken und zum Betreiben von Flugzeughilfsgeräten |
US4046335A (en) * | 1975-06-26 | 1977-09-06 | Helmut Osberger | Helicopters safety drive |
SE7611617L (sv) * | 1976-10-20 | 1978-04-21 | Kronogard Sven Olof | Fordonsmaskineri |
US4257281A (en) * | 1979-06-25 | 1981-03-24 | The Bendix Corporation | Engine starter and accessory drive apparatus |
US4514976A (en) * | 1980-06-02 | 1985-05-07 | Rockwell International Corporation | Integrated auxiliary power and environmental control unit |
GB2076897B (en) * | 1980-06-02 | 1983-06-29 | Rockwell International Corp | Integrated auxiliary and environmental control unit |
DE3515770A1 (de) * | 1985-05-02 | 1986-11-06 | Klöckner-Humboldt-Deutz AG, 5000 Köln | Hilfsantriebsanordnung mit getriebe fuer ein gasturbinentriebwerk |
US4829850A (en) * | 1987-02-25 | 1989-05-16 | Soloy Dual Pac, Inc. | Multiple engine drive for single output shaft and combining gearbox therefor |
US4864812A (en) * | 1987-11-13 | 1989-09-12 | Sundstrand Corporation | Combined auxiliary and emergency power unit |
US4914906A (en) * | 1988-05-24 | 1990-04-10 | Allied-Signal Inc. | Turbine starter device |
US5309708A (en) * | 1988-06-03 | 1994-05-10 | Alliedsignal Inc. | Multifunction integrated power unit |
-
1990
- 1990-09-24 US US07/587,709 patent/US5201798A/en not_active Expired - Lifetime
-
1991
- 1991-09-05 EP EP91918486A patent/EP0550658B1/de not_active Expired - Lifetime
- 1991-09-05 DE DE69105146T patent/DE69105146T2/de not_active Expired - Lifetime
- 1991-09-05 WO PCT/US1991/006344 patent/WO1992005351A1/en active IP Right Grant
Also Published As
Publication number | Publication date |
---|---|
EP0550658A1 (de) | 1993-07-14 |
WO1992005351A1 (en) | 1992-04-02 |
EP0550658B1 (de) | 1994-11-09 |
US5201798A (en) | 1993-04-13 |
DE69105146T2 (de) | 1995-04-13 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |