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ZA200610305B - Driving system for auxiliary machines of a double-body turbo engine - Google Patents

Driving system for auxiliary machines of a double-body turbo engine

Info

Publication number
ZA200610305B
ZA200610305B ZA200610305A ZA200610305A ZA200610305B ZA 200610305 B ZA200610305 B ZA 200610305B ZA 200610305 A ZA200610305 A ZA 200610305A ZA 200610305 A ZA200610305 A ZA 200610305A ZA 200610305 B ZA200610305 B ZA 200610305B
Authority
ZA
South Africa
Prior art keywords
double
driving system
auxiliary machines
turbo engine
body turbo
Prior art date
Application number
ZA200610305A
Other languages
English (en)
Inventor
Linet Hugues Henri Raymond
Pettinotti Serge Dominique
Mouchnino Cyril Franck
Original Assignee
Hispano Suiza Sa
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 Hispano Suiza Sa filed Critical Hispano Suiza Sa
Publication of ZA200610305B publication Critical patent/ZA200610305B/xx

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00—Pumping installations or systems
    • F04D25/02—Units comprising pumps and their driving means
    • F04D25/04—Units comprising pumps and their driving means the pump being fluid-driven
    • 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
    • F02C3/107—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission
    • F02C3/113—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission with variable power transmission between 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
    • 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
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Structure Of Transmissions (AREA)
  • Supercharger (AREA)
  • General Details Of Gearings (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
ZA200610305A 2005-12-09 2006-12-08 Driving system for auxiliary machines of a double-body turbo engine ZA200610305B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0553816A FR2894621B1 (fr) 2005-12-09 2005-12-09 Systeme d'entrainement de machines auxiliaires d'un turbomoteur a double corps

Publications (1)

Publication Number Publication Date
ZA200610305B true ZA200610305B (en) 2008-08-27

Family

ID=36941970

Family Applications (1)

Application Number Title Priority Date Filing Date
ZA200610305A ZA200610305B (en) 2005-12-09 2006-12-08 Driving system for auxiliary machines of a double-body turbo engine

Country Status (10)

Country Link
US (1) US7690185B2 (xx)
EP (1) EP1798399B1 (xx)
JP (1) JP4918341B2 (xx)
CA (1) CA2569948C (xx)
FR (1) FR2894621B1 (xx)
IL (1) IL179928A (xx)
PL (1) PL1798399T3 (xx)
RU (1) RU2429360C2 (xx)
UA (1) UA92893C2 (xx)
ZA (1) ZA200610305B (xx)

Families Citing this family (45)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7942079B2 (en) 2007-02-16 2011-05-17 Hamilton Sundstrand Corporation Multi-speed gearbox for low spool driven auxiliary component
FR2921423B1 (fr) * 2007-09-25 2014-04-25 Snecma Turbomachine a double corps, avec double prelevement de puissance
US20090188334A1 (en) * 2008-01-25 2009-07-30 United Technologies Corp. Accessory Gearboxes and Related Gas Turbine Engine Systems
US8146370B2 (en) * 2008-05-21 2012-04-03 Honeywell International Inc. Turbine drive system with lock-up clutch and method
FR2932850B1 (fr) * 2008-06-23 2010-08-13 Snecma Procede et systeme de determination de la position angulaire d'un rotor de turboreacteur.
FR2937088B1 (fr) * 2008-10-13 2013-07-12 Snecma Distribution de fluide dans une turbomachine
US9816441B2 (en) * 2009-03-30 2017-11-14 United Technologies Corporation Gas turbine engine with stacked accessory components
US20120006137A1 (en) * 2010-07-07 2012-01-12 Hamilton Sundstrand Corporation Gear driven accessory for gearbox
EP2696058B1 (en) 2011-04-07 2017-10-11 Kawasaki Jukogyo Kabushiki Kaisha Aircraft with a generator apparatus
US8814502B2 (en) 2011-05-31 2014-08-26 Pratt & Whitney Canada Corp. Dual input drive AGB for gas turbine engines
US8561503B2 (en) * 2011-07-28 2013-10-22 Hamilton Sundstrand Corporation Motor-generator and prime mover gearing assembly
US8943839B2 (en) * 2011-08-26 2015-02-03 United Technologies Corporation Gas turbine engine generator switchable drive
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
GB201219544D0 (en) * 2012-10-31 2012-12-12 Rolls Royce Deutschland Geared compressor for gas turbine engine
US9316159B2 (en) 2013-01-30 2016-04-19 Pratt & Whitney Canada Corp. Gas turbine engine with transmission
US9752500B2 (en) 2013-03-14 2017-09-05 Pratt & Whitney Canada Corp. Gas turbine engine with transmission and method of adjusting rotational speed
US9347373B2 (en) * 2013-12-19 2016-05-24 Pratt & Whitney Canada Corp. Gas turbine engine with transmission
US9869190B2 (en) 2014-05-30 2018-01-16 General Electric Company Variable-pitch rotor with remote counterweights
US10072510B2 (en) 2014-11-21 2018-09-11 General Electric Company Variable pitch fan for gas turbine engine and method of assembling the same
US10100653B2 (en) 2015-10-08 2018-10-16 General Electric Company Variable pitch fan blade retention system
US11415063B2 (en) 2016-09-15 2022-08-16 Pratt & Whitney Canada Corp. Reverse-flow gas turbine engine
US10883424B2 (en) 2016-07-19 2021-01-05 Pratt & Whitney Canada Corp. Multi-spool gas turbine engine architecture
US11035293B2 (en) 2016-09-15 2021-06-15 Pratt & Whitney Canada Corp. Reverse flow gas turbine engine with offset RGB
US10465611B2 (en) 2016-09-15 2019-11-05 Pratt & Whitney Canada Corp. Reverse flow multi-spool gas turbine engine with aft-end accessory gearbox drivingly connected to both high pressure spool and low pressure spool
RU2644497C1 (ru) * 2016-11-15 2018-02-12 Публичное акционерное общество "ОДК - Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Единый механизм передачи крутящего момента агрегатам газотурбинного двигателя (варианты)
US10815899B2 (en) 2016-11-15 2020-10-27 Pratt & Whitney Canada Corp. Gas turbine engine accessories arrangement
RU2634505C1 (ru) * 2016-12-09 2017-10-31 Публичное Акционерное Общество "Уфимское Моторостроительное Производственное Объединение" (Пао "Умпо") Способ управления двухроторным газотурбинным двигателем самолета в режиме запуска при авторотации
RU2630927C1 (ru) * 2016-12-29 2017-09-14 Публичное Акционерное Общество "Уфимское Моторостроительное Производственное Объединение" (Пао "Умпо") Способ работы коробки двигательных агрегатов (КДА) двухвального двухконтурного турбореактивного двигателя (ТРД) и КДА, работающая этим способом; способ работы насоса-регулятора КДА ТРД и насос-регулятор, работающий этим способом; способ работы форсажного насоса КДА ТРД -и форсажный насос, работающий этим способом; способ работы суфлёра центробежного КДА ТРД и суфлёр центробежный, работающий этим способом
RU2630928C1 (ru) * 2016-12-29 2017-09-14 Публичное Акционерное Общество "Уфимское Моторостроительное Производственное Объединение" (Пао "Умпо") Способ работы коробки двигательных агрегатов (КДА) двухвального двухконтурного турбореактивного двигателя (ТРД); способ работы насоса плунжерного КДА ТРД и насос плунжерный, работающий этим способом; способ работы двигательного центробежного насоса КДА ТРД и двигательный центробежный насос, работающий этим способом; способ работы маслоагрегата КДА ТРД и маслоагрегат, работающий этим способом
US10590852B2 (en) * 2017-01-19 2020-03-17 United Technologies Corporation Gas turbine engine dual towershaft accessory gearbox assembly with a transmission
US10995673B2 (en) 2017-01-19 2021-05-04 Raytheon Technologies Corporation Gas turbine engine with intercooled cooling air and dual towershaft accessory gearbox
US10590853B2 (en) * 2017-01-19 2020-03-17 United Technologies Corporation Gas turbine engine dual towershaft accessory gearbox assembly with a transmission
US10808624B2 (en) 2017-02-09 2020-10-20 Pratt & Whitney Canada Corp. Turbine rotor with low over-speed requirements
US10738709B2 (en) 2017-02-09 2020-08-11 Pratt & Whitney Canada Corp. Multi-spool gas turbine engine
RU2639260C1 (ru) * 2017-02-16 2017-12-20 Публичное акционерное общество "ОДК - Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Способ управления двухроторным газотурбинным двигателем
US10746188B2 (en) 2017-03-14 2020-08-18 Pratt & Whitney Canada Corp. Inter-shaft bearing connected to a compressor boost system
CA3051563A1 (en) 2018-08-08 2020-02-08 Pratt & Whitney Canada Corp. Turboshaft gas turbine engine
US10890115B2 (en) * 2018-09-28 2021-01-12 Raytheon Technologies Corporation Low torque engine starting with dual spool power extraction with superposition gearbox
EP3885563B1 (en) * 2018-11-19 2024-08-28 Kawasaki Jukogyo Kabushiki Kaisha Electric power generation controller for use in aircraft and electric power generating apparatus including same
GB201913195D0 (en) * 2019-09-12 2019-10-30 Rolls Royce Plc Gas turbine engine
US11248523B2 (en) * 2019-11-06 2022-02-15 Raytheon Technologies Corporation Dual clutch transmission for accessory gearbox drive
US11739694B2 (en) * 2020-04-15 2023-08-29 General Electric Company Embedded electric motor assembly
US12084195B2 (en) 2021-04-29 2024-09-10 Hamilton Sundstrand Corporation Dual drive, dual clutch drive system for an aircraft accessory
US11674435B2 (en) 2021-06-29 2023-06-13 General Electric Company Levered counterweight feathering system
US11795964B2 (en) 2021-07-16 2023-10-24 General Electric Company Levered counterweight feathering system

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US3100378A (en) * 1960-11-14 1963-08-13 Avco Corp Auxiliary power drive mechanism for a gas turbine engine
GB1092745A (en) * 1965-10-11 1967-11-29 Dowty Rotol Ltd Engine installations and starting means therefore
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
FR2076589A5 (xx) * 1970-01-20 1971-10-15 Kronogard Sven Olof
US3899877A (en) * 1973-07-02 1975-08-19 Gen Motors Corp Gas turbine engine power shift transmission power train
US4018316A (en) * 1974-03-07 1977-04-19 General Motors Corporation Engine and transmission power train
SE439337B (sv) * 1980-09-29 1985-06-10 Volvo Ab Gasturbinmaskineri
US4699021A (en) * 1984-09-20 1987-10-13 Avco Corporation Integrated power system
US4912921A (en) * 1988-03-14 1990-04-03 Sundstrand Corporation Low speed spool emergency power extraction system
GB9313905D0 (en) * 1993-07-06 1993-08-25 Rolls Royce Plc Shaft power transfer in gas turbine engines
GB9606546D0 (en) * 1996-03-28 1996-06-05 Rolls Royce Plc Gas turbine engine system
US6142418A (en) * 1998-05-12 2000-11-07 Hamilton Sundstrand Corporation Multi-path secondary power system for an aircraft

Also Published As

Publication number Publication date
JP2007162688A (ja) 2007-06-28
EP1798399A1 (fr) 2007-06-20
JP4918341B2 (ja) 2012-04-18
CA2569948C (fr) 2014-05-13
IL179928A0 (en) 2007-05-15
EP1798399B1 (fr) 2015-05-06
UA92893C2 (uk) 2010-12-27
US7690185B2 (en) 2010-04-06
FR2894621A1 (fr) 2007-06-15
FR2894621B1 (fr) 2011-10-14
RU2429360C2 (ru) 2011-09-20
US20070130959A1 (en) 2007-06-14
PL1798399T3 (pl) 2015-10-30
CA2569948A1 (fr) 2007-06-09
RU2006143720A (ru) 2008-06-27
IL179928A (en) 2010-12-30

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