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FR3007461B1 - Procede et systeme de demarrage d'une turbomachine d'aeronef. - Google Patents

Procede et systeme de demarrage d'une turbomachine d'aeronef.

Info

Publication number
FR3007461B1
FR3007461B1 FR1356054A FR1356054A FR3007461B1 FR 3007461 B1 FR3007461 B1 FR 3007461B1 FR 1356054 A FR1356054 A FR 1356054A FR 1356054 A FR1356054 A FR 1356054A FR 3007461 B1 FR3007461 B1 FR 3007461B1
Authority
FR
France
Prior art keywords
starting
aircraft turbomachine
turbomachine
aircraft
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
FR1356054A
Other languages
English (en)
Other versions
FR3007461A1 (fr
Inventor
Patrick Zaccaria
Philippe Chareyre
Pio Fernandez-Lopez
Carlos Casado-Montero
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.)
Airbus Operations SL
Airbus Operations SAS
General Electric Co
Original Assignee
Airbus Operations SL
Airbus Operations SAS
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 Airbus Operations SL, Airbus Operations SAS filed Critical Airbus Operations SL
Priority to FR1356054A priority Critical patent/FR3007461B1/fr
Priority to US14/314,752 priority patent/US10125690B2/en
Publication of FR3007461A1 publication Critical patent/FR3007461A1/fr
Application granted granted Critical
Publication of FR3007461B1 publication Critical patent/FR3007461B1/fr
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
    • F02C7/26—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
    • 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
    • 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)
    • 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
    • F05D2260/85—Starting
    • 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
    • F05D2260/96—Preventing, counteracting or reducing vibration or noise
    • 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
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/11—Purpose of the control system to prolong engine life
    • F05D2270/114—Purpose of the control system to prolong engine life by limiting mechanical stresses
    • 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
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/304—Spool rotational speed

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
FR1356054A 2013-06-25 2013-06-25 Procede et systeme de demarrage d'une turbomachine d'aeronef. Active FR3007461B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1356054A FR3007461B1 (fr) 2013-06-25 2013-06-25 Procede et systeme de demarrage d'une turbomachine d'aeronef.
US14/314,752 US10125690B2 (en) 2013-06-25 2014-06-25 Method and system for starting up an aircraft turbomachine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1356054A FR3007461B1 (fr) 2013-06-25 2013-06-25 Procede et systeme de demarrage d'une turbomachine d'aeronef.

Publications (2)

Publication Number Publication Date
FR3007461A1 FR3007461A1 (fr) 2014-12-26
FR3007461B1 true FR3007461B1 (fr) 2015-07-17

Family

ID=49111437

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1356054A Active FR3007461B1 (fr) 2013-06-25 2013-06-25 Procede et systeme de demarrage d'une turbomachine d'aeronef.

Country Status (2)

Country Link
US (1) US10125690B2 (fr)
FR (1) FR3007461B1 (fr)

Families Citing this family (68)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3007460B1 (fr) 2013-06-25 2015-07-17 Airbus Operations Sas Procede et systeme de demarrage d'une turbomachine d'aeronef par regulation en temps reel de debit d'air.
FR3011581B1 (fr) * 2013-10-08 2018-08-24 Continental Automotive France Procede de compensation d'un signal d'un dispositif de mesure de pression au sein d'un moteur a combustion interne
US10502139B2 (en) 2015-01-28 2019-12-10 General Electric Company Method of starting a gas turbine engine including a cooling phase
US11149642B2 (en) 2015-12-30 2021-10-19 General Electric Company System and method of reducing post-shutdown engine temperatures
US10125691B2 (en) 2016-02-12 2018-11-13 United Technologies Corporation Bowed rotor start using a variable position starter valve
US10174678B2 (en) 2016-02-12 2019-01-08 United Technologies Corporation Bowed rotor start using direct temperature measurement
US10125636B2 (en) 2016-02-12 2018-11-13 United Technologies Corporation Bowed rotor prevention system using waste heat
US10443505B2 (en) 2016-02-12 2019-10-15 United Technologies Corporation Bowed rotor start mitigation in a gas turbine engine
US10436064B2 (en) 2016-02-12 2019-10-08 United Technologies Corporation Bowed rotor start response damping system
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
US20170234235A1 (en) * 2016-02-12 2017-08-17 Hamilton Sundstrand Corporation Electro-pneumatic gas turbine engine motoring system for bowed rotor engine starts
US9664070B1 (en) 2016-02-12 2017-05-30 United Technologies Corporation Bowed rotor prevention system
US10040577B2 (en) * 2016-02-12 2018-08-07 United Technologies Corporation Modified start sequence of a gas turbine engine
US10443507B2 (en) 2016-02-12 2019-10-15 United Technologies Corporation Gas turbine engine bowed rotor avoidance system
US10508601B2 (en) * 2016-02-12 2019-12-17 United Technologies Corporation Auxiliary drive bowed rotor prevention system for a gas turbine engine
US10539079B2 (en) 2016-02-12 2020-01-21 United Technologies Corporation Bowed rotor start mitigation in a gas turbine engine using aircraft-derived parameters
FR3047771A1 (fr) * 2016-02-16 2017-08-18 Airbus Operations Sas Systeme et procede de demarrage des moteurs d'un aeronef bimoteur
US10598047B2 (en) 2016-02-29 2020-03-24 United Technologies Corporation Low-power bowed rotor prevention system
US10337405B2 (en) 2016-05-17 2019-07-02 General Electric Company Method and system for bowed rotor start mitigation using rotor cooling
US10563590B2 (en) * 2016-05-19 2020-02-18 Hamilton Sundstrand Corporation System and method of gas turbine engine shaft cooling
US10724443B2 (en) 2016-05-24 2020-07-28 General Electric Company Turbine engine and method of operating
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
US10480417B2 (en) 2016-07-14 2019-11-19 Hamilton Sundstrand Corporation Air turbine start system
EP3273006B1 (fr) 2016-07-21 2019-07-03 United Technologies Corporation Démarrage en alternance d'un groupe bi-moteur
US10221774B2 (en) 2016-07-21 2019-03-05 United Technologies Corporation Speed control during motoring of a gas turbine engine
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
EP3273016B1 (fr) 2016-07-21 2020-04-01 United Technologies Corporation Coordination multimoteur pendant la motorisation de moteur à turbine à gaz
FR3055358B1 (fr) * 2016-08-25 2018-08-17 Safran Aircraft Engines Procede de gestion d'une panne de vanne de demarrage d'une turbomachine
US10787968B2 (en) * 2016-09-30 2020-09-29 Raytheon Technologies Corporation Gas turbine engine motoring with starter air valve manual override
US10583933B2 (en) 2016-10-03 2020-03-10 General Electric Company Method and apparatus for undercowl flow diversion cooling
US10598095B2 (en) 2016-10-11 2020-03-24 Unison Industries, Llc Integrated starter for aerial vehicle
US10266278B2 (en) * 2016-10-11 2019-04-23 Unison Industries, Llc Starter issue detection
US20180112600A1 (en) * 2016-10-21 2018-04-26 Hamilton Sundstrand Corporation Starter air valve system with regulating bleed
US10443543B2 (en) 2016-11-04 2019-10-15 United Technologies Corporation High compressor build clearance reduction
EP3324021B1 (fr) * 2016-11-21 2021-03-03 Airbus Operations, S.L. Aéronef intégrant un système de démarrage de moteur principal
US10823079B2 (en) * 2016-11-29 2020-11-03 Raytheon Technologies Corporation Metered orifice for motoring of a gas turbine engine
US10301963B2 (en) 2016-12-28 2019-05-28 Hamilton Sundstrand Corporation Starter air valve systems configured for low speed motoring
US10669945B2 (en) * 2017-02-06 2020-06-02 Raytheon Technologies Corporation Starter air valve system with dual electromechanical controls
US11022004B2 (en) 2017-03-31 2021-06-01 The Boeing Company Engine shaft integrated motor
US10753225B2 (en) * 2017-03-31 2020-08-25 The Boeing Company Engine turning motor via pneumatic or hydraulic motor
US10378442B2 (en) 2017-03-31 2019-08-13 The Boeing Company Mechanical flywheel for bowed rotor mitigation
US10427632B2 (en) 2017-03-31 2019-10-01 The Boeing Company Bowed rotor nacelle cooling
US20180334963A1 (en) * 2017-05-22 2018-11-22 General Electric Company Systems and methods for bowed rotor start mitigation
US20190040799A1 (en) * 2017-08-07 2019-02-07 United Technologies Corporation System and method for rotating a gas turbine engine during a motoring cycle
US10947993B2 (en) 2017-11-27 2021-03-16 General Electric Company Thermal gradient attenuation structure to mitigate rotor bow in turbine engine
US10781754B2 (en) * 2017-12-08 2020-09-22 Pratt & Whitney Canada Corp. System and method for rotor bow mitigation
US11549392B2 (en) 2017-12-14 2023-01-10 General Electric Company Structure and method to mitigate rotor bow in turbine engine
US10718231B2 (en) * 2017-12-15 2020-07-21 General Electric Company Method and system for mitigating bowed rotor operation of gas turbine engine
GB201720944D0 (en) * 2017-12-15 2018-01-31 Rolls Royce Plc Rotor bow management
US11162428B2 (en) 2017-12-18 2021-11-02 General Electric Company Method of starting a gas turbine engine
US10760498B2 (en) 2018-01-04 2020-09-01 General Electric Company System and method for removing rotor bow in a gas turbine engine using mechanical energy storage device
US11162419B2 (en) * 2018-02-12 2021-11-02 General Electric Company Method and structure for operating engine with bowed rotor condition
US11339721B2 (en) 2018-11-14 2022-05-24 Honeywell International Inc. System and method for supplying compressed air to a main engine starter motor
US11199139B2 (en) * 2018-12-19 2021-12-14 Raytheon Technologies Corporation Gas turbine engine system bowed rotor start mitigation and wear reduction
US11306654B2 (en) 2018-12-19 2022-04-19 Raytheon Technologies Corporation Gas turbine engine system wear reduction
US11274599B2 (en) 2019-03-27 2022-03-15 Pratt & Whitney Canada Corp. Air system switching system to allow aero-engines to operate in standby mode
US11859563B2 (en) * 2019-05-31 2024-01-02 Pratt & Whitney Canada Corp. Air system of multi-engine aircraft
US11274611B2 (en) 2019-05-31 2022-03-15 Pratt & Whitney Canada Corp. Control logic for gas turbine engine fuel economy
US20200385133A1 (en) * 2019-06-06 2020-12-10 Gulfstream Aerospace Corporation Engine and thrust control of aircraft in no dwell zone
US11486310B2 (en) 2020-03-27 2022-11-01 Pratt & Whitney Canada Corp. System and method for dynamic engine motoring
US11668248B2 (en) 2020-03-27 2023-06-06 Pratt & Whitney Canada Corp. Start-up system and method for rotor bow mitigation
US11359546B2 (en) * 2020-04-20 2022-06-14 Honeywell International Inc. System and method for controlling engine speed with bowed rotor mitigation
US11702952B2 (en) * 2021-11-11 2023-07-18 General Electric Company Thermal bias control in turbomachines
US11879411B2 (en) 2022-04-07 2024-01-23 General Electric Company System and method for mitigating bowed rotor in a gas turbine engine
US12078105B2 (en) * 2022-06-14 2024-09-03 General Electric Company System and method for providing cooling in a compressor section of a gas turbine engine
CN116906190B (zh) * 2023-09-14 2023-12-05 中国航发上海商用航空发动机制造有限责任公司 一种航空发动机冷运转控制系统和方法

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4473752A (en) 1982-05-27 1984-09-25 Lockheed Corporation Aircraft engine starting with synchronous ac generator
US4627234A (en) * 1983-06-15 1986-12-09 Sundstrand Corporation Gas turbine engine/load compressor power plants
US5127220A (en) * 1991-02-28 1992-07-07 Allied-Signal Inc. Method for accelerating a gas turbine engine
GB2348466B (en) 1999-03-27 2003-07-09 Rolls Royce Plc A gas turbine engine and a rotor for a gas turbine engine
US6684898B2 (en) * 2001-09-27 2004-02-03 Honeywell International Inc. Dual actuator air turbine starter valve
EP1835131A1 (fr) * 2006-03-15 2007-09-19 Siemens Aktiengesellschaft Turbine à gas pour une centrale thermique et procédé de fonctionnement d'une telle turbine
US20100085676A1 (en) 2008-10-03 2010-04-08 Honeywell International Inc. Nested pulse width modulation control
FR2947006B1 (fr) * 2009-06-17 2014-10-17 Eurocopter France Dispositif et procede pour le demarrage d'un moteur a turbine equipant un helicoptere,mettant en oeuvre une source d'energie electrique comprenant des organes d'appoint a decharge
US8820046B2 (en) 2009-10-05 2014-09-02 General Electric Company Methods and systems for mitigating distortion of gas turbine shaft
US8555653B2 (en) * 2009-12-23 2013-10-15 General Electric Company Method for starting a turbomachine
US9845734B2 (en) * 2011-04-20 2017-12-19 Honeywell International Inc. Air turbine start system with monopole starter air valve position
FR2977915B1 (fr) * 2011-07-12 2018-11-16 Safran Helicopter Engines Procede de demarrage d'une turbomachine reduisant le balourd thermique
FR3007459B1 (fr) * 2013-06-19 2016-10-14 Airbus Operations Sas Systeme et procede de mise en rotation d'un element rotatif d'un dispositif mecanique, en particulier d'une turbomachine.
FR3007460B1 (fr) 2013-06-25 2015-07-17 Airbus Operations Sas Procede et systeme de demarrage d'une turbomachine d'aeronef par regulation en temps reel de debit d'air.
US9567906B2 (en) * 2013-12-13 2017-02-14 Honeywell International Inc. Systems and methods for controlling aircraft main engine speeds by adjusting compressed air flow from an APU
FR3022949B1 (fr) * 2014-06-26 2016-07-15 Snecma Procedes de determination de caracteristiques d'ouvertures ou de fermetures d'une vanne de demarrage de turbomoteur

Also Published As

Publication number Publication date
FR3007461A1 (fr) 2014-12-26
US20140373553A1 (en) 2014-12-25
US10125690B2 (en) 2018-11-13

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