DE602005009879D1 - Mechanisches Antriebssystem für ein Hilfsaggregats-Getriebe - Google Patents

Mechanisches Antriebssystem für ein Hilfsaggregats-Getriebe

Info

Publication number
DE602005009879D1
DE602005009879D1 DE602005009879T DE602005009879T DE602005009879D1 DE 602005009879 D1 DE602005009879 D1 DE 602005009879D1 DE 602005009879 T DE602005009879 T DE 602005009879T DE 602005009879 T DE602005009879 T DE 602005009879T DE 602005009879 D1 DE602005009879 D1 DE 602005009879D1
Authority
DE
Germany
Prior art keywords
drive system
mechanical drive
auxiliary gearing
gearing
auxiliary
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
Application number
DE602005009879T
Other languages
English (en)
Inventor
Guy W Miller
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.)
RTX Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of DE602005009879D1 publication Critical patent/DE602005009879D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • 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
    • F05D2260/00—Function
    • F05D2260/40—Transmission of power
    • F05D2260/403—Transmission of power through the shape of the drive components
    • F05D2260/4031—Transmission of power through the shape of the drive components as in toothed gearing
    • 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
    • F05D2260/00—Function
    • F05D2260/50—Kinematic linkage, i.e. transmission of position
    • F05D2260/53—Kinematic linkage, i.e. transmission of position using gears
    • 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
    • Y10T74/19642—Directly cooperating gears
    • Y10T74/19674—Spur and bevel

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gear Transmission (AREA)
DE602005009879T 2004-02-25 2005-02-24 Mechanisches Antriebssystem für ein Hilfsaggregats-Getriebe Active DE602005009879D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/785,502 US7386983B2 (en) 2004-02-25 2004-02-25 Apparatus for driving an accessory gearbox in a gas turbine engine

Publications (1)

Publication Number Publication Date
DE602005009879D1 true DE602005009879D1 (de) 2008-11-06

Family

ID=34827566

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005009879T Active DE602005009879D1 (de) 2004-02-25 2005-02-24 Mechanisches Antriebssystem für ein Hilfsaggregats-Getriebe

Country Status (4)

Country Link
US (1) US7386983B2 (de)
EP (1) EP1574688B1 (de)
JP (1) JP2005240800A (de)
DE (1) DE602005009879D1 (de)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2882096B1 (fr) * 2005-02-11 2012-04-20 Snecma Moteurs Turbomoteur a double corps avec des moyens de prise de mouvement sur les rotors basse pression et haute pression, module de prise de mouvement pour le turbomoteur et procede de montage du turbomoteur
FR2892456B1 (fr) * 2005-10-21 2008-01-04 Hispano Suiza Sa Dispositif d'entrainement de machines accessoires d'un moteur a turbine a gaz
FR2892455B1 (fr) * 2005-10-21 2008-01-04 Hispano Suiza Sa Dispositif d'entrainement de machines auxiliaires d'un turbomoteur a double corps
FR2901315B1 (fr) * 2006-05-19 2010-09-10 Hispano Suiza Sa Boitier d'accessoires dans un moteur d'avion tel qu'un turboreacteur
US8590151B2 (en) * 2006-06-30 2013-11-26 Solar Turbines Inc. System for supporting and servicing a gas turbine engine
US8672606B2 (en) * 2006-06-30 2014-03-18 Solar Turbines Inc. Gas turbine engine and system for servicing a gas turbine engine
US20080187431A1 (en) * 2006-06-30 2008-08-07 Ian Trevor Brown Power system
US7997085B2 (en) * 2006-09-27 2011-08-16 General Electric Company Gas turbine engine assembly and method of assembling same
US7788898B2 (en) * 2006-12-06 2010-09-07 General Electric Company Variable coupling of turbofan engine spools via open differential gear set or simple planetary gear set for improved power extraction and engine operability, with torque coupling for added flexibility
WO2008082334A1 (en) * 2006-12-29 2008-07-10 Volvo Aero Corporation A gas turbine engine, an aircraft provided therewith, and a method of controlling the operation of such an engine
FR2921423B1 (fr) * 2007-09-25 2014-04-25 Snecma Turbomachine a double corps, avec double prelevement de puissance
US9719428B2 (en) * 2007-11-30 2017-08-01 United Technologies Corporation Gas turbine engine with pylon mounted accessory drive
US20090188334A1 (en) * 2008-01-25 2009-07-30 United Technologies Corp. Accessory Gearboxes and Related Gas Turbine Engine Systems
US20090205341A1 (en) * 2008-02-20 2009-08-20 Muldoon Marc J Gas turbine engine with twin towershaft accessory gearbox
US8480527B2 (en) * 2008-08-27 2013-07-09 Rolls-Royce Corporation Gearing arrangement
FR2942273B1 (fr) * 2009-02-18 2011-06-10 Snecma Moteur double flux a roues de turbine contrarotatives
US9816441B2 (en) * 2009-03-30 2017-11-14 United Technologies Corporation Gas turbine engine with stacked accessory components
US8572974B2 (en) * 2009-07-31 2013-11-05 Hamilton Sundstrand Corporation Variable speed and displacement electric fluid delivery system for a gas turbine engine
JP5703370B2 (ja) * 2011-04-07 2015-04-15 川崎重工業株式会社 航空機用発電装置
US8814502B2 (en) 2011-05-31 2014-08-26 Pratt & Whitney Canada Corp. Dual input drive AGB for gas turbine engines
FR2976976B1 (fr) 2011-06-24 2013-06-28 Snecma Relais d'accessoires a duree de vie amelioree
US9068515B2 (en) 2011-12-07 2015-06-30 United Technologies Corporation Accessory gearbox with tower shaft removal capability
US20130180262A1 (en) * 2012-01-18 2013-07-18 Hung Duong Gas turbine engine accessory gearbox
US8973465B2 (en) 2012-07-20 2015-03-10 United Technologies Corporation Gearbox for gas turbine engine
US9297314B2 (en) 2012-12-19 2016-03-29 United Technologies Corporation Gas turbine engine with accessory gear box
US10641181B2 (en) 2013-01-30 2020-05-05 United Technologies Corporation Gas turbine engine accessory gearbox
ITTO20130636A1 (it) * 2013-07-29 2015-01-30 Avio Spa Scatola di trasmissione, e metodo di smontaggio per disaccoppiare un albero di azionamento in tale scatola di trasmissione
US10197150B2 (en) 2015-11-23 2019-02-05 United Technologies Corporation Gear baffle configured with lubricant outlet passage
US10221937B2 (en) 2016-04-05 2019-03-05 United Technologies Corporation Slotted oil baffle for gears
US10364880B2 (en) 2017-01-05 2019-07-30 United Technologies Corporation Oil quieting direction control baffle
US10655679B2 (en) 2017-04-07 2020-05-19 United Technologies Corporation Oil control for seal plates
US10677159B2 (en) 2017-10-27 2020-06-09 General Electric Company Gas turbine engine including a dual-speed split compressor
US10823081B2 (en) 2017-12-21 2020-11-03 Raytheon Technologies Corporation Concentric power takeoff transmission
US10920671B2 (en) 2018-09-25 2021-02-16 Raytheon Technologies Corporation Thrust balance control with differential power extraction
US20200256430A1 (en) * 2019-02-13 2020-08-13 United Technologies Corporation Angle accessory gearbox for gas turbine engine
GB2610565A (en) 2021-09-08 2023-03-15 Rolls Royce Plc An improved gas turbine engine
GB2610568A (en) 2021-09-08 2023-03-15 Rolls Royce Plc An improved gas turbine engine
GB2610567A (en) 2021-09-08 2023-03-15 Rolls Royce Plc An improved gas turbine engine
GB2610569A (en) 2021-09-08 2023-03-15 Rolls Royce Plc An improved gas turbine engine
GB2610571A (en) 2021-09-08 2023-03-15 Rolls Royce Plc An improved gas turbine engine
GB2610572A (en) * 2021-09-08 2023-03-15 Rolls Royce Plc An improved gas turbine engine

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB839961A (en) * 1956-11-01 1960-06-29 Bristol Siddeley Engines Ltd Improvements in or relating to engine accessory mounting arrangements
US2952973A (en) * 1958-06-02 1960-09-20 Gen Motors Corp Turbofan-ramjet engine
GB1055118A (en) * 1965-08-19 1967-01-18 Rolls Royce Gas turbine engine accessory drive mechanism
US3543588A (en) * 1968-11-12 1970-12-01 Gen Motors Corp Accessory installation
US4525995A (en) * 1983-04-04 1985-07-02 Williams International Corporation Oil scavening system for gas turbine engine
DE3622022A1 (de) * 1986-07-01 1988-01-07 Kloeckner Humboldt Deutz Ag Gasturbinentriebwerk
US5309708A (en) * 1988-06-03 1994-05-10 Alliedsignal Inc. Multifunction integrated power unit
GB9313905D0 (en) * 1993-07-06 1993-08-25 Rolls Royce Plc Shaft power transfer in gas turbine engines
US20050183540A1 (en) * 2004-02-25 2005-08-25 Miller Guy W. Apparatus for driving an accessory gearbox in a gas turbine engine

Also Published As

Publication number Publication date
US7386983B2 (en) 2008-06-17
US20050183529A1 (en) 2005-08-25
EP1574688B1 (de) 2008-09-24
EP1574688A1 (de) 2005-09-14
JP2005240800A (ja) 2005-09-08

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