FR2908461B1 - Generateur de secours a turboreacteur a double flux - Google Patents
Generateur de secours a turboreacteur a double flux Download PDFInfo
- Publication number
- FR2908461B1 FR2908461B1 FR0707910A FR0707910A FR2908461B1 FR 2908461 B1 FR2908461 B1 FR 2908461B1 FR 0707910 A FR0707910 A FR 0707910A FR 0707910 A FR0707910 A FR 0707910A FR 2908461 B1 FR2908461 B1 FR 2908461B1
- Authority
- FR
- France
- Prior art keywords
- turboreactor
- double flow
- relief generator
- relief
- generator
- 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.)
- Active
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
-
- 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
- F02C7/262—Restarting after flame-out
-
- 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
- F05D2220/30—Application in turbines
- F05D2220/34—Application in turbines in ram-air turbines ("RATS")
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US11598482 | 2006-11-13 | ||
US11/598,482 US7841163B2 (en) | 2006-11-13 | 2006-11-13 | Turbofan emergency generator |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2908461A1 FR2908461A1 (fr) | 2008-05-16 |
FR2908461B1 true FR2908461B1 (fr) | 2018-04-20 |
Family
ID=38896234
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0707910A Active FR2908461B1 (fr) | 2006-11-13 | 2007-11-12 | Generateur de secours a turboreacteur a double flux |
Country Status (3)
Country | Link |
---|---|
US (1) | US7841163B2 (fr) |
FR (1) | FR2908461B1 (fr) |
GB (1) | GB2443743B (fr) |
Families Citing this family (60)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20140174056A1 (en) | 2008-06-02 | 2014-06-26 | United Technologies Corporation | Gas turbine engine with low stage count low pressure turbine |
US8128021B2 (en) | 2008-06-02 | 2012-03-06 | United Technologies Corporation | Engine mount system for a turbofan gas turbine engine |
FR2946091A1 (fr) * | 2009-10-16 | 2010-12-03 | Snecma | Turbomachine d'aeronef comprenant un generateur electrique de puissance agence de facon inclinee dans le compartiment inter-veine |
FR2953199B1 (fr) * | 2009-12-02 | 2012-02-24 | Hispano Suiza Sa | Alterno-demarreur de moteur aeronautique entraine par un train epicycloidal |
US8424800B2 (en) | 2010-06-23 | 2013-04-23 | Hamilton Sundstrand Corporation | Multi-source emergency power optimization |
US8425372B2 (en) | 2010-07-14 | 2013-04-23 | Hamilton Sundstrand Corporation | Geared turbofan emergency power |
IT1401662B1 (it) | 2010-08-27 | 2013-08-02 | Nuova Pignone S R L | Dispositivo espansore multistadio assiale con ingranaggi, sistema e metodo. |
US8519555B2 (en) * | 2010-11-29 | 2013-08-27 | Pratt & Whitney Canada Corp. | Combination low spool generator and ram air turbine generator |
EP2492451B1 (fr) * | 2011-02-28 | 2021-05-19 | Hamilton Sundstrand Corporation | Aéronef avec générateur d'urgence couplé à un arbre basse pression |
US9188105B2 (en) | 2011-04-19 | 2015-11-17 | Hamilton Sundstrand Corporation | Strut driveshaft for ram air turbine |
US9523422B2 (en) | 2011-06-08 | 2016-12-20 | United Technologies Corporation | Flexible support structure for a geared architecture gas turbine engine |
US8814503B2 (en) | 2011-06-08 | 2014-08-26 | United Technologies Corporation | Flexible support structure for a geared architecture gas turbine engine |
US8297916B1 (en) | 2011-06-08 | 2012-10-30 | United Technologies Corporation | Flexible support structure for a geared architecture gas turbine engine |
US9631558B2 (en) | 2012-01-03 | 2017-04-25 | United Technologies Corporation | Geared architecture for high speed and small volume fan drive turbine |
US9133729B1 (en) | 2011-06-08 | 2015-09-15 | United Technologies Corporation | Flexible support structure for a geared architecture gas turbine engine |
US8770922B2 (en) | 2011-06-08 | 2014-07-08 | United Technologies Corporation | Flexible support structure for a geared architecture gas turbine engine |
US9239012B2 (en) | 2011-06-08 | 2016-01-19 | United Technologies Corporation | Flexible support structure for a geared architecture gas turbine engine |
US8678310B2 (en) | 2011-08-22 | 2014-03-25 | Honeywell International Inc. | Ducted ram air generator assembly |
DE102011112255A1 (de) | 2011-09-02 | 2013-03-07 | Rolls-Royce Deutschland Ltd & Co Kg | Hilfsgerätegetriebeeinrichtung für ein Triebwerk |
US9267438B2 (en) | 2011-10-11 | 2016-02-23 | Pratt & Whitney Canada Corp. | Starting of aircraft engine |
US8966876B2 (en) | 2011-10-21 | 2015-03-03 | United Technologies Corporation | Controllable speed windmill operation of a gas turbine engine through low spool power extraction |
US9003811B2 (en) | 2011-11-28 | 2015-04-14 | Pratt & Whitney Canada Corp. | Support for electric machine in a turbine engine |
US9429077B2 (en) | 2011-12-06 | 2016-08-30 | Pratt & Whitney Canada Corp. | Multiple turboshaft engine control method and system for helicopters |
US10125693B2 (en) | 2012-04-02 | 2018-11-13 | United Technologies Corporation | Geared turbofan engine with power density range |
JP5568596B2 (ja) * | 2012-05-30 | 2014-08-06 | 川崎重工業株式会社 | 航空機用エンジンのギヤボックス一体型発電装置 |
US8756908B2 (en) | 2012-05-31 | 2014-06-24 | United Technologies Corporation | Fundamental gear system architecture |
US8572943B1 (en) | 2012-05-31 | 2013-11-05 | United Technologies Corporation | Fundamental gear system architecture |
US20150308351A1 (en) | 2012-05-31 | 2015-10-29 | United Technologies Corporation | Fundamental gear system architecture |
US9097134B2 (en) | 2012-09-14 | 2015-08-04 | Pratt & Whitney Canada Corp. | Air cooling design for tail-cone generator installation |
US9297422B2 (en) | 2012-10-25 | 2016-03-29 | Pratt & Whitney Canada Corp. | Coupling element for torque transmission in a gas turbine engine |
GB201219916D0 (en) | 2012-11-06 | 2012-12-19 | Rolls Royce Plc | An electrical generation arrangement for an aircraft |
US9371739B2 (en) * | 2013-01-04 | 2016-06-21 | Raytheon Company | Power producing device with control mechanism |
US10316745B2 (en) | 2013-02-26 | 2019-06-11 | United Technologies Corporation | Turbomachine fan clutch |
EP3882448B1 (fr) | 2013-03-12 | 2024-07-10 | RTX Corporation | Accouplement flexible pour turbine à engrenages |
US9517843B2 (en) | 2013-03-13 | 2016-12-13 | Rolls-Royce North American Technologies, Inc. | Generator for flight vehicle |
EP3080424B1 (fr) * | 2013-12-13 | 2022-05-04 | Raytheon Technologies Corporation | Architecture pour un système de propulsion axialement compact et à performances élevées |
FR3020410B1 (fr) | 2014-04-29 | 2021-09-17 | Snecma | Turbomachine d'aeronef a prelevement de puissance mecanique ameliore |
US9915164B2 (en) * | 2014-05-20 | 2018-03-13 | United Technologies Corporation | Geared turbofan with high speed generator |
GB201420105D0 (en) * | 2014-11-12 | 2014-12-24 | Rolls Royce Plc | Gas turbine electrical machine arrangement |
US20160348589A1 (en) * | 2014-11-24 | 2016-12-01 | Hamilton Sundstrand Corporation | Aircraft engine assembly and method of generating electric energy for an aircraft power system |
US10119465B2 (en) | 2015-06-23 | 2018-11-06 | United Technologies Corporation | Geared turbofan with independent flexible ring gears and oil collectors |
GB2550397B (en) * | 2016-05-19 | 2018-11-21 | Derwent Aviation Consulting Ltd | A turbo machine comprising a compressor system |
US11131208B2 (en) * | 2016-09-01 | 2021-09-28 | Rolls-Royce North American Technologies, Inc. | Embedded electric generator in turbine engine |
US10738692B2 (en) | 2017-09-20 | 2020-08-11 | Honeywell International Inc. | Distributed propulsion and electric power generation system |
US11156128B2 (en) * | 2018-08-22 | 2021-10-26 | General Electric Company | Embedded electric machine |
US11097849B2 (en) | 2018-09-10 | 2021-08-24 | General Electric Company | Aircraft having an aft engine |
US11081917B2 (en) | 2018-11-29 | 2021-08-03 | General Electric Company | Electric machine and a turbo machine having the same |
US11434778B2 (en) | 2019-03-11 | 2022-09-06 | Hamilton Sundstrand Corporation | Integrated tail cone and mounted generator acoustic suppression |
US11319895B2 (en) | 2019-03-15 | 2022-05-03 | Hamilton Sundstrand Corporation | Integrated tail cone and mounted generator |
US11242156B2 (en) * | 2019-03-15 | 2022-02-08 | Hamilton Sundstrand Corporation | Plug in fluid cooled electrical connections for tail cone mounted generator |
GB201910008D0 (en) | 2019-07-12 | 2019-08-28 | Rolls Royce Plc | Gas turbine engine electrical generator |
GB201910010D0 (en) | 2019-07-12 | 2019-08-28 | Rolls Royce Plc | Gas turbine engine electrical generator |
GB201910009D0 (en) | 2019-07-12 | 2019-08-28 | Rolls Royce Plc | Gas turbine engine electrical generator |
GB201910011D0 (en) * | 2019-07-12 | 2019-08-28 | Rolls Royce Plc | Gas turbine engine electrical generator |
JP7416081B2 (ja) * | 2019-09-30 | 2024-01-17 | 株式会社Ihi | 発電機及び当該発電機を備える航空機用多軸式ガスタービンエンジン |
FR3110931B1 (fr) * | 2020-05-27 | 2022-06-10 | Safran Trans Systems | Turbomachine equipee d’une machine electrique montee en serie avec un reducteur de vitesse |
US20220352836A1 (en) * | 2021-04-29 | 2022-11-03 | Hamilton Sundstrand Corporation | Aircraft engine system including a clutch and motor controller for selectively connecting a generator and a turbine engine |
US11719119B1 (en) | 2022-03-23 | 2023-08-08 | Rolls-Royce Corporation | Aircraft with ram air turbine disk with generator having blade shroud ring integrated magnets |
US11878812B2 (en) | 2022-03-23 | 2024-01-23 | Rolls-Royce Corporation | Aircraft accessory unit powered by ram air turbine |
US20230387750A1 (en) * | 2022-05-31 | 2023-11-30 | Pratt & Whitney Canada Corp. | Gas turbine engine with electric machine in engine core |
Family Cites Families (26)
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US2953900A (en) * | 1955-10-10 | 1960-09-27 | Nathan C Price | Combined open-cycle closed-cycle powerplant for aircraft |
NO150135C (no) | 1982-05-10 | 1984-08-22 | Kongsberg Vapenfab As | Anordning ved ramluftturbiner |
US4692093A (en) | 1982-05-28 | 1987-09-08 | The Garrett Corporation | Ram air turbine |
US4671737A (en) | 1984-12-26 | 1987-06-09 | Sundstrand Corporation | Blade pitch changing mechanism |
EP0210175A1 (fr) | 1985-01-24 | 1987-02-04 | Sundstrand Corporation | Turbine a air dynamique |
US4743163A (en) | 1985-11-22 | 1988-05-10 | Sundstrand Corporation | Ram air turbine control system |
US4701104A (en) | 1986-06-18 | 1987-10-20 | Sundstrand Corporation | Ram air turbine |
US4864812A (en) * | 1987-11-13 | 1989-09-12 | Sundstrand Corporation | Combined auxiliary and emergency power unit |
US4912921A (en) * | 1988-03-14 | 1990-04-03 | Sundstrand Corporation | Low speed spool emergency power extraction system |
IT1219726B (it) | 1988-06-15 | 1990-05-24 | Fimac Spa | Turbina ad elevato rendimento,in particolare per lo sfruttamento di energia eolica per sorgenti ausiliarie di energia in impieghi aeronautici |
US5687561A (en) | 1991-09-17 | 1997-11-18 | Rolls-Royce Plc | Ducted fan gas turbine engine accessory drive |
GB9119852D0 (en) | 1991-09-17 | 1991-10-30 | Rolls Royce Plc | Ducted fan gas turbine engine accessory drive system |
US5249924A (en) | 1992-02-21 | 1993-10-05 | Southwest Aerospace Corporation | RAM air turbine |
GB9313905D0 (en) | 1993-07-06 | 1993-08-25 | Rolls Royce Plc | Shaft power transfer in gas turbine engines |
US5564903A (en) | 1993-11-23 | 1996-10-15 | Alliedsignal Inc. | In-line ram air turbine power system |
US5558495A (en) | 1993-12-02 | 1996-09-24 | Sundstrand Corporation | Electromagnetic heating devices, particularly for ram air turbines |
US5562417A (en) | 1994-08-10 | 1996-10-08 | Sundstrand Corporation | Control mechanism for RAM air turbine |
US5779446A (en) | 1995-11-07 | 1998-07-14 | Sundstrand Corporation | Air driven turbine including a blade pitch control system |
GB9606546D0 (en) | 1996-03-28 | 1996-06-05 | Rolls Royce Plc | Gas turbine engine system |
US5845483A (en) | 1996-04-10 | 1998-12-08 | General Electric Company | Windmill engine starting system with fluid driven motor and pump |
US6127758A (en) | 1997-09-17 | 2000-10-03 | Alliedsignal Inc. | Ram air turbine system |
IL143755A0 (en) | 1998-12-14 | 2002-04-21 | Ghetzler Aero Power Corp | Low drag ducted ram air turbine generator and cooling system |
GB9910393D0 (en) * | 1999-05-05 | 1999-07-07 | Lucas Ind Plc | Electrical generator,an aero-engine including such a generator and an aircraft including such a generator |
GB0313563D0 (en) | 2003-06-12 | 2003-07-16 | Smiths Group Plc | Ram air turbines |
US6943478B2 (en) * | 2003-11-14 | 2005-09-13 | Dura-Trac Motors, Inc. | Brushless permanent magnet wheel motor with variable axial rotor/stator alignment |
US7055303B2 (en) * | 2003-12-22 | 2006-06-06 | Pratt & Whitney Canada Corp. | Gas turbine engine architecture |
-
2006
- 2006-11-13 US US11/598,482 patent/US7841163B2/en active Active
-
2007
- 2007-11-12 FR FR0707910A patent/FR2908461B1/fr active Active
- 2007-11-13 GB GB0722280A patent/GB2443743B/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR2908461A1 (fr) | 2008-05-16 |
GB0722280D0 (en) | 2007-12-27 |
US7841163B2 (en) | 2010-11-30 |
GB2443743B (en) | 2009-04-29 |
US20080110151A1 (en) | 2008-05-15 |
GB2443743A (en) | 2008-05-14 |
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