ES2026486T3 - Mecanismo propulsor de turbina de gas. - Google Patents

Mecanismo propulsor de turbina de gas.

Info

Publication number
ES2026486T3
ES2026486T3 ES198787109380T ES87109380T ES2026486T3 ES 2026486 T3 ES2026486 T3 ES 2026486T3 ES 198787109380 T ES198787109380 T ES 198787109380T ES 87109380 T ES87109380 T ES 87109380T ES 2026486 T3 ES2026486 T3 ES 2026486T3
Authority
ES
Spain
Prior art keywords
gas turbine
propeller mechanism
turbine propeller
pressure rotor
impeller
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
Application number
ES198787109380T
Other languages
English (en)
Inventor
Heinz Brockmann
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.)
Rolls Royce Deutschland Ltd and Co KG
Original Assignee
BMW Rolls Royce 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 BMW Rolls Royce GmbH filed Critical BMW Rolls Royce GmbH
Application granted granted Critical
Publication of ES2026486T3 publication Critical patent/ES2026486T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F02C7/36—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
    • 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
    • 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
    • F05D2260/402—Transmission of power through friction drives
    • F05D2260/4023—Transmission of power through friction drives through a friction clutch
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

SE PROPONE UN PROPULSOR DE TURBINA DE GAS (1) EN QUE EL IMPULSOR AUXILIAR (17) PUEDE ACOPLARSE CON EL ROTOR DE PRESION INFERIOR (2) O CON EL ROTOR DE PRESION SUPERIOR (3).
ES198787109380T 1986-07-01 1987-06-30 Mecanismo propulsor de turbina de gas. Expired - Lifetime ES2026486T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19863622022 DE3622022A1 (de) 1986-07-01 1986-07-01 Gasturbinentriebwerk

Publications (1)

Publication Number Publication Date
ES2026486T3 true ES2026486T3 (es) 1992-05-01

Family

ID=6304130

Family Applications (1)

Application Number Title Priority Date Filing Date
ES198787109380T Expired - Lifetime ES2026486T3 (es) 1986-07-01 1987-06-30 Mecanismo propulsor de turbina de gas.

Country Status (4)

Country Link
US (1) US4776163A (es)
EP (1) EP0251289B1 (es)
DE (2) DE3622022A1 (es)
ES (1) ES2026486T3 (es)

Families Citing this family (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4912921A (en) * 1988-03-14 1990-04-03 Sundstrand Corporation Low speed spool emergency power extraction system
FR2826052B1 (fr) * 2001-06-19 2003-12-19 Snecma Moteurs Dispositif de secours au rallumage d'un turboreacteur en autorotation
US6735954B2 (en) * 2001-12-21 2004-05-18 Pratt & Whitney Canada Corp. Offset drive for gas turbine engine
US20070199331A1 (en) * 2003-09-19 2007-08-30 Maguire Alan R Power transmission arrangement
FR2863312B1 (fr) * 2003-12-09 2008-07-04 Snecma Moteurs Turboreacteur a double corps avec moyen d'entrainement des machines accessoires
US20050183540A1 (en) * 2004-02-25 2005-08-25 Miller Guy W. Apparatus for driving an accessory gearbox in a gas turbine engine
US7055330B2 (en) * 2004-02-25 2006-06-06 United Technologies Corp Apparatus for driving an accessory gearbox in a gas turbine engine
US7386983B2 (en) * 2004-02-25 2008-06-17 United Technologies Corporation Apparatus for driving an accessory gearbox in a gas turbine engine
FR2880920B1 (fr) 2005-01-20 2007-07-06 Snecma Moteurs Sa Turbomoteur a double corps avec des moyens d'entrainement du boitier d'accessoires
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
US20070022735A1 (en) * 2005-07-29 2007-02-01 General Electric Company Pto assembly for a gas turbine engine
FR2892455B1 (fr) * 2005-10-21 2008-01-04 Hispano Suiza Sa Dispositif d'entrainement de machines auxiliaires d'un turbomoteur a double corps
US7861533B2 (en) * 2006-04-21 2011-01-04 Pratt & Whitney Canada Corp Relighting a turbofan engine
FR2903451B1 (fr) * 2006-07-07 2008-09-12 Snecma Sa Turbomoteur avec un alternateur et procede de transmission de mouvement a un alternateur
DE102006039608A1 (de) * 2006-08-24 2008-04-10 Rolls-Royce Deutschland Ltd & Co Kg Anordnung zur Energieentnahme bei einem Zwei-Wellen-Triebwerk
US7997085B2 (en) * 2006-09-27 2011-08-16 General Electric Company Gas turbine engine assembly and method of assembling same
WO2008045074A1 (en) * 2006-10-12 2008-04-17 United Technologies Corporation Turbofan engine with variable bypass nozzle exit area and method of operation
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
US7942079B2 (en) * 2007-02-16 2011-05-17 Hamilton Sundstrand Corporation Multi-speed gearbox for low spool driven auxiliary component
FR2915523A1 (fr) * 2007-04-27 2008-10-31 Snecma Sa Dispositif de production d'energie electrique dans un moteur a turbine a gaz a double corps
US7882691B2 (en) * 2007-07-05 2011-02-08 Hamilton Sundstrand Corporation High to low pressure spool summing gearbox for accessory power extraction and electric start
FR2921423B1 (fr) * 2007-09-25 2014-04-25 Snecma Turbomachine a double corps, avec double prelevement de puissance
US8333554B2 (en) * 2007-11-14 2012-12-18 United Technologies Corporation Split gearbox and nacelle arrangement
WO2009067048A1 (en) * 2007-11-20 2009-05-28 Volvo Aero Corporation Gas turbine engine
DE102008031185A1 (de) * 2008-07-03 2010-01-07 Rolls-Royce Deutschland Ltd & Co Kg Turbofantriebwerk mit mindestens einer Vorrichtung zum Antreiben mindestens eines Generators
US7963094B1 (en) * 2010-01-19 2011-06-21 Cupolo Francis J Fragmentor for bird ingestible gas turbine engine
US8690099B2 (en) * 2010-11-16 2014-04-08 Rolls-Royce Corporation Aircraft and propulsion system
US8814502B2 (en) 2011-05-31 2014-08-26 Pratt & Whitney Canada Corp. Dual input drive AGB for gas turbine engines
US20130247539A1 (en) * 2012-03-26 2013-09-26 Richard John Hoppe Multi-shaft power extraction from gas turbine engine
FR3026787B1 (fr) * 2014-10-07 2019-04-19 Safran Transmission Systems Transmission spinale compacte
US20170107845A1 (en) * 2015-10-15 2017-04-20 General Electric Company Systems and methods to facilitate enhancing turbine output using an auxiliary generator
US10767568B2 (en) * 2018-09-11 2020-09-08 Raytheon Technologies Corporation Dual spool power extraction with superposition gearbox
US10890115B2 (en) * 2018-09-28 2021-01-12 Raytheon Technologies Corporation Low torque engine starting with dual spool power extraction with superposition gearbox
US11346427B2 (en) * 2019-02-13 2022-05-31 Raytheon Technologies Corporation Accessory gearbox for gas turbine engine with variable transmission
US11248523B2 (en) 2019-11-06 2022-02-15 Raytheon Technologies Corporation Dual clutch transmission for accessory gearbox drive
US11591967B2 (en) * 2020-12-21 2023-02-28 The Boeing Company Systems and methods for providing mechanical power to an aircraft accessory with a turbine engine
US12084195B2 (en) 2021-04-29 2024-09-10 Hamilton Sundstrand Corporation Dual drive, dual clutch drive system for an aircraft accessory

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2696711A (en) * 1948-08-13 1954-12-14 Bristol Aeroplane Co Ltd Gas turbine engine and the starting thereof
GB703262A (en) * 1950-10-16 1954-02-03 Rolls Royce Improvements in or relating to gas-turbine engines
US2823320A (en) * 1953-11-23 1958-02-11 Larsson Carl Folke Power producing unit
US2803943A (en) * 1953-12-30 1957-08-27 Armstrong Siddeley Motors Ltd Means for supporting and driving accessories which are exterior to a ductedfan turbo-jet engine
DE1031058B (de) * 1955-06-22 1958-05-29 Bristol Aero Engines Ltd Propellerantreibende Gasturbine
US3100378A (en) * 1960-11-14 1963-08-13 Avco Corp Auxiliary power drive mechanism for a gas turbine engine
GB973388A (en) * 1963-05-24 1964-10-28 George Garnham Turner Accessory power drive mechanism for a gas turbine engine
FR1360218A (fr) * 1963-03-07 1964-05-08 Gen Motors Corp Groupe moteur à turbine à gaz
US3514945A (en) * 1968-10-04 1970-06-02 Avco Corp Gas turbine accessory power drive unit
US3680309A (en) * 1969-09-25 1972-08-01 Garrett Corp Two-spool auxiliary power unit and control means
CH520266A (de) * 1970-01-21 1972-03-15 Kronogard Sven Olof Gasturbinentriebwerk
US3626692A (en) * 1970-04-15 1971-12-14 Garrett Corp Gas turbine power plant
DE3143389A1 (de) * 1981-11-02 1983-08-25 Roland Fahrzeugplanung und -Vertrieb GmbH, 8000 München Kombinationstriebwerk fuer schwere landfahrzeuge

Also Published As

Publication number Publication date
DE3622022A1 (de) 1988-01-07
US4776163A (en) 1988-10-11
EP0251289A3 (en) 1989-11-15
EP0251289A2 (de) 1988-01-07
DE3773763D1 (de) 1991-11-21
EP0251289B1 (de) 1991-10-16

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