JP2015520821A5 - - Google Patents

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Publication number
JP2015520821A5
JP2015520821A5 JP2015507577A JP2015507577A JP2015520821A5 JP 2015520821 A5 JP2015520821 A5 JP 2015520821A5 JP 2015507577 A JP2015507577 A JP 2015507577A JP 2015507577 A JP2015507577 A JP 2015507577A JP 2015520821 A5 JP2015520821 A5 JP 2015520821A5
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JP
Japan
Prior art keywords
motor
gas
shaft
positive displacement
emergency start
Prior art date
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Granted
Application number
JP2015507577A
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English (en)
Japanese (ja)
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JP6208216B2 (ja
JP2015520821A (ja
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Publication date
Priority claimed from FR1253938A external-priority patent/FR2990004B1/fr
Application filed filed Critical
Publication of JP2015520821A publication Critical patent/JP2015520821A/ja
Publication of JP2015520821A5 publication Critical patent/JP2015520821A5/ja
Application granted granted Critical
Publication of JP6208216B2 publication Critical patent/JP6208216B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2015507577A 2012-04-27 2013-04-18 エネルギー発電設備の緊急起動の方法およびシステム Expired - Fee Related JP6208216B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1253938A FR2990004B1 (fr) 2012-04-27 2012-04-27 Procede et systeme de demarrage d'urgence d'architecture generatrice d'energie
FR1253938 2012-04-27
PCT/FR2013/050863 WO2013160590A1 (fr) 2012-04-27 2013-04-18 Procédé et système de démarrage d'urgence d'architecture génératrice d'énergie

Publications (3)

Publication Number Publication Date
JP2015520821A JP2015520821A (ja) 2015-07-23
JP2015520821A5 true JP2015520821A5 (https=) 2017-09-28
JP6208216B2 JP6208216B2 (ja) 2017-10-04

Family

ID=46826641

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2015507577A Expired - Fee Related JP6208216B2 (ja) 2012-04-27 2013-04-18 エネルギー発電設備の緊急起動の方法およびシステム

Country Status (12)

Country Link
US (1) US10072580B2 (https=)
EP (1) EP2841742B1 (https=)
JP (1) JP6208216B2 (https=)
KR (1) KR102049130B1 (https=)
CN (1) CN104246181B (https=)
CA (1) CA2869361C (https=)
ES (1) ES2572093T3 (https=)
FR (1) FR2990004B1 (https=)
IN (1) IN2014DN08865A (https=)
PL (1) PL2841742T3 (https=)
RU (1) RU2621190C2 (https=)
WO (1) WO2013160590A1 (https=)

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FR3017417B1 (fr) * 2014-02-10 2018-10-26 Safran Helicopter Engines Dispositif pyrotechnique pour l'entrainement d'une machine tournante
FR3019524B1 (fr) * 2014-04-03 2017-12-08 Turbomeca Chaine motrice pour helicoptere incorporant un module moteur pyrotechnique d'assistance et helicoptere la comportant
FR3019588B1 (fr) 2014-04-08 2019-06-14 Safran Helicopter Engines Dispositif d'assistance d'un systeme propulsif a propergol solide d'un helicoptere monomoteur, helicoptere monomoteur comprenant un tel dispositif et procede correspondant
FR3027346B1 (fr) * 2014-10-20 2019-08-09 Safran Helicopter Engines Pack amovible de reactivation d'un turbomoteur, architecture d'un systeme propulsif d'un helicoptere multi-moteur equipe d'un tel pack et helicoptere correspondant
US10054008B2 (en) * 2015-02-09 2018-08-21 United Technologies Corporation Turbomachine accessory gearbox bracket
FR3033882B1 (fr) * 2015-03-16 2017-04-07 Herakles Generateur de gaz
US10539079B2 (en) 2016-02-12 2020-01-21 United Technologies Corporation Bowed rotor start mitigation in a gas turbine engine using aircraft-derived parameters
US10443505B2 (en) 2016-02-12 2019-10-15 United Technologies Corporation Bowed rotor start mitigation in a gas turbine engine
US10443507B2 (en) 2016-02-12 2019-10-15 United Technologies Corporation Gas turbine engine bowed rotor avoidance system
US9664070B1 (en) 2016-02-12 2017-05-30 United Technologies Corporation Bowed rotor prevention system
US10125636B2 (en) 2016-02-12 2018-11-13 United Technologies Corporation Bowed rotor prevention system using waste heat
US10040577B2 (en) 2016-02-12 2018-08-07 United Technologies Corporation Modified start sequence of a gas turbine engine
US10436064B2 (en) 2016-02-12 2019-10-08 United Technologies Corporation Bowed rotor start response damping system
US10125691B2 (en) 2016-02-12 2018-11-13 United Technologies Corporation Bowed rotor start using a variable position starter valve
US10508601B2 (en) 2016-02-12 2019-12-17 United Technologies Corporation Auxiliary drive bowed rotor prevention system for a gas turbine engine
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
US10174678B2 (en) 2016-02-12 2019-01-08 United Technologies Corporation Bowed rotor start using direct temperature measurement
EP3211184B1 (en) 2016-02-29 2021-05-05 Raytheon Technologies Corporation Bowed rotor prevention system and associated method of bowed rotor prevention
CN107404147A (zh) * 2016-05-20 2017-11-28 北京汽车股份有限公司 汽车及其应急启动发电装置
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
US10384791B2 (en) 2016-07-21 2019-08-20 United Technologies Corporation Cross engine coordination during gas turbine engine motoring
US10618666B2 (en) 2016-07-21 2020-04-14 United Technologies Corporation Pre-start motoring synchronization for multiple engines
US10221774B2 (en) 2016-07-21 2019-03-05 United Technologies Corporation Speed control during motoring of a gas turbine engine
EP3273006B1 (en) 2016-07-21 2019-07-03 United Technologies Corporation Alternating starter use during multi-engine motoring
EP3273016B1 (en) 2016-07-21 2020-04-01 United Technologies Corporation Multi-engine coordination during gas turbine engine motoring
US10787968B2 (en) 2016-09-30 2020-09-29 Raytheon Technologies Corporation Gas turbine engine motoring with starter air valve manual override
US10443543B2 (en) 2016-11-04 2019-10-15 United Technologies Corporation High compressor build clearance reduction
US10823079B2 (en) 2016-11-29 2020-11-03 Raytheon Technologies Corporation Metered orifice for motoring of a gas turbine engine
CN110291282B (zh) * 2016-12-15 2021-12-31 通用电气航空系统有限责任公司 具有分离器的空气涡轮启动器
US10823080B2 (en) 2017-05-31 2020-11-03 General Electric Company Dual accessory gearbox
FR3082225B1 (fr) 2018-06-07 2020-06-05 Safran Helicopter Engines Systeme propulsif asymetrique a recuperation de chaleur
US11512645B2 (en) * 2020-03-06 2022-11-29 Goodrich Corporation Solid-propellant gas generator assemblies and methods

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FR1104252A (fr) * 1954-05-06 1955-11-17 Snecma Démarreur amovible destiné notamment aux moteurs d'aviation
US2942415A (en) * 1954-11-29 1960-06-28 Bayard Gaston System for feeding gases into a starting turbine
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FR1303228A (fr) * 1961-08-29 1962-09-07 Sundstrand A G Démarreur pour moteurs
FR1334270A (fr) * 1962-09-25 1963-08-02 Cessna Aircraft Co Moteur actionné par un fluide sous pression
US3633360A (en) * 1970-01-20 1972-01-11 Talley Industries Boost starter system
FR2475127A1 (fr) * 1980-02-06 1981-08-07 Snecma Generateur de gaz a variation de volume
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FR2897895A1 (fr) * 2006-02-27 2007-08-31 Hispano Suiza Sa Integration d'un demarreur/generateur dans une boite de transmission d'une turbine a gaz
FR2914697B1 (fr) * 2007-04-06 2012-11-30 Turbomeca Dispositif d'assistance aux phases transitoires d'acceleration et de deceleration
US8148834B2 (en) * 2009-05-19 2012-04-03 General Electric Company Aircraft engine starting/generating system and method of control

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