RU2621190C2 - Способ и система экстренного запуска установки генерирования энергии - Google Patents

Способ и система экстренного запуска установки генерирования энергии Download PDF

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Publication number
RU2621190C2
RU2621190C2 RU2014142446A RU2014142446A RU2621190C2 RU 2621190 C2 RU2621190 C2 RU 2621190C2 RU 2014142446 A RU2014142446 A RU 2014142446A RU 2014142446 A RU2014142446 A RU 2014142446A RU 2621190 C2 RU2621190 C2 RU 2621190C2
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RU
Russia
Prior art keywords
engine
shaft
installation
emergency start
gases
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RU2014142446A
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English (en)
Russian (ru)
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RU2014142446A (ru
Inventor
Юг ФИЛИПЮТТИ
Франк ГАРД
Ромэн ТИРЬЕ
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Турбомека
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Publication of RU2014142446A publication Critical patent/RU2014142446A/ru
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Publication of RU2621190C2 publication Critical patent/RU2621190C2/ru

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    • 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
    • F02C7/27—Fluid drives
    • F02C7/272—Fluid drives generated by cartridges
    • 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
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02N—STARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
    • F02N13/00—Starting of engines, or driving of starting apparatus by use of explosives, e.g. stored in cartridges
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02N—STARTING OF COMBUSTION ENGINES; STARTING AIDS FOR SUCH ENGINES, NOT OTHERWISE PROVIDED FOR
    • F02N15/00—Other power-operated starting apparatus; Component parts, details, or accessories, not provided for in, or of interest apart from groups F02N5/00 - F02N13/00
    • F02N15/10—Safety devices not otherwise provided for
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Automotive Seat Belt Assembly (AREA)
  • Control Of Eletrric Generators (AREA)
RU2014142446A 2012-04-27 2013-04-18 Способ и система экстренного запуска установки генерирования энергии RU2621190C2 (ru)

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 (2)

Publication Number Publication Date
RU2014142446A RU2014142446A (ru) 2016-06-20
RU2621190C2 true RU2621190C2 (ru) 2017-06-01

Family

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Family Applications (1)

Application Number Title Priority Date Filing Date
RU2014142446A RU2621190C2 (ru) 2012-04-27 2013-04-18 Способ и система экстренного запуска установки генерирования энергии

Country Status (12)

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

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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
US10508601B2 (en) 2016-02-12 2019-12-17 United Technologies Corporation Auxiliary drive bowed rotor prevention system for a gas turbine engine
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
US10125636B2 (en) 2016-02-12 2018-11-13 United Technologies Corporation Bowed rotor prevention system using waste heat
US10436064B2 (en) 2016-02-12 2019-10-08 United Technologies Corporation Bowed rotor start response damping system
US10174678B2 (en) 2016-02-12 2019-01-08 United Technologies Corporation Bowed rotor start using direct temperature measurement
US10443505B2 (en) 2016-02-12 2019-10-15 United Technologies Corporation Bowed rotor start mitigation in a gas turbine engine
US10125691B2 (en) 2016-02-12 2018-11-13 United Technologies Corporation Bowed rotor start using a variable position starter valve
US10539079B2 (en) 2016-02-12 2020-01-21 United Technologies Corporation Bowed rotor start mitigation in a gas turbine engine using aircraft-derived parameters
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
US10443507B2 (en) 2016-02-12 2019-10-15 United Technologies Corporation Gas turbine engine bowed rotor avoidance system
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
EP3273016B1 (en) 2016-07-21 2020-04-01 United Technologies Corporation Multi-engine coordination during gas turbine engine motoring
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
EP3273006B1 (en) 2016-07-21 2019-07-03 United Technologies Corporation Alternating starter use during multi-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
US11333078B2 (en) 2016-12-15 2022-05-17 Ge Aviation Systems Llc Air turbine starter with decoupler
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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Publication number Priority date Publication date Assignee Title
FR1104252A (fr) * 1954-05-06 1955-11-17 Snecma Démarreur amovible destiné notamment aux moteurs d'aviation
FR1126010A (fr) * 1955-05-09 1956-11-13 Air Equipement Perfectionnements aux démarreurs à turbine
US2942415A (en) * 1954-11-29 1960-06-28 Bayard Gaston System for feeding gases into a starting turbine
FR1334270A (fr) * 1962-09-25 1963-08-02 Cessna Aircraft Co Moteur actionné par un fluide sous pression
RU2275957C1 (ru) * 2004-09-13 2006-05-10 Российская Федерация, от имени которой выступает Государственный заказчик - Федеральное агентство по атомной энергии Устройство для генерирования газа

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FR1303228A (fr) * 1961-08-29 1962-09-07 Sundstrand A G Démarreur pour moteurs
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
US6931856B2 (en) * 2003-09-12 2005-08-23 Mes International, Inc. Multi-spool turbogenerator system and control method
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

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
FR1126010A (fr) * 1955-05-09 1956-11-13 Air Equipement Perfectionnements aux démarreurs à turbine
FR1334270A (fr) * 1962-09-25 1963-08-02 Cessna Aircraft Co Moteur actionné par un fluide sous pression
RU2275957C1 (ru) * 2004-09-13 2006-05-10 Российская Федерация, от имени которой выступает Государственный заказчик - Федеральное агентство по атомной энергии Устройство для генерирования газа

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Title
АЛАБИН М.А. Запуск авиационных газотурбинных двигателей, М.: Машиностроение, 1968, с.22-23, с.37-39. *

Also Published As

Publication number Publication date
IN2014DN08865A (enExample) 2015-05-22
RU2014142446A (ru) 2016-06-20
ES2572093T3 (es) 2016-05-30
US20150128592A1 (en) 2015-05-14
CN104246181A (zh) 2014-12-24
KR102049130B1 (ko) 2019-11-26
KR20150003189A (ko) 2015-01-08
CA2869361C (fr) 2020-06-30
JP6208216B2 (ja) 2017-10-04
JP2015520821A (ja) 2015-07-23
PL2841742T3 (pl) 2016-08-31
CA2869361A1 (fr) 2013-10-31
CN104246181B (zh) 2016-06-22
WO2013160590A1 (fr) 2013-10-31
EP2841742B1 (fr) 2016-03-30
FR2990004B1 (fr) 2014-04-18
FR2990004A1 (fr) 2013-11-01
US10072580B2 (en) 2018-09-11
EP2841742A1 (fr) 2015-03-04

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