ES2572093T3 - Procedimiento y sistema de arranque de emergencia para estructura generatriz de energía - Google Patents

Procedimiento y sistema de arranque de emergencia para estructura generatriz de energía

Info

Publication number
ES2572093T3
ES2572093T3 ES13722505T ES13722505T ES2572093T3 ES 2572093 T3 ES2572093 T3 ES 2572093T3 ES 13722505 T ES13722505 T ES 13722505T ES 13722505 T ES13722505 T ES 13722505T ES 2572093 T3 ES2572093 T3 ES 2572093T3
Authority
ES
Spain
Prior art keywords
emergency start
volumetric
connection
procedure
motor
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
ES13722505T
Other languages
English (en)
Spanish (es)
Inventor
Hugues Filiputti
Franck Garde
Romain Thiriet
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.)
Safran Helicopter Engines SAS
Original Assignee
Turbomeca SA
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 Turbomeca SA filed Critical Turbomeca SA
Application granted granted Critical
Publication of ES2572093T3 publication Critical patent/ES2572093T3/es
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
    • F02C7/27—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

Landscapes

  • 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)
ES13722505T 2012-04-27 2013-04-18 Procedimiento y sistema de arranque de emergencia para estructura generatriz de energía Active ES2572093T3 (es)

Applications Claiming Priority (2)

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
PCT/FR2013/050863 WO2013160590A1 (fr) 2012-04-27 2013-04-18 Procédé et système de démarrage d'urgence d'architecture génératrice d'énergie

Publications (1)

Publication Number Publication Date
ES2572093T3 true ES2572093T3 (es) 2016-05-30

Family

ID=46826641

Family Applications (1)

Application Number Title Priority Date Filing Date
ES13722505T Active ES2572093T3 (es) 2012-04-27 2013-04-18 Procedimiento y sistema de arranque de emergencia para estructura generatriz de energía

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)

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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

Family Cites Families (12)

* 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
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
US6931856B2 (en) * 2003-09-12 2005-08-23 Mes International, Inc. Multi-spool turbogenerator system and control method
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
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

Also Published As

Publication number Publication date
IN2014DN08865A (enExample) 2015-05-22
RU2014142446A (ru) 2016-06-20
RU2621190C2 (ru) 2017-06-01
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

Similar Documents

Publication Publication Date Title
ES2572093T3 (es) Procedimiento y sistema de arranque de emergencia para estructura generatriz de energía
MX2021004414A (es) Maquina que comprende un tren motriz hibrido y metodo de control correspondiente.
BR112014007149A2 (pt) sistema híbrido de volante
BR112017018148A2 (pt) dispositivo para geração de força de propulsão e aeronave
CL2013002408A1 (es) Aparato de generación de potencia de las olas, que comprende; un flotador, una unidad de transmisión de potencia, un generador, un mecanismo de retorno, donde una cuerda de transmisión de potencia, una cuerda de retorno y un eje de transmisión de potencia, están acoplados por la unidad de transmisión de potencia.
BR112014013877A8 (pt) retardador hidrodinâmico e método para acionar o mesmo
CL2016000245A1 (es) Aparato de conversion de potencia para sistemas de generacion mareomotriz que comprende un arbol de entrada, un arbol de transmision de energia conectado a medios de almacenamiento de energia y un arbol de salida, en donde el arbol de salida recibe potencia desde el arbol de entrada y el arbol de transmision de energia.
MX2017012950A (es) Dispositivo para controlar el arranque de un vehiculo electricamente accionado.
IN266774B (enExample)
CL2017003022A1 (es) Sistemas, métodos y aparatos para almacenamiento de energía en una máquina minera.
CL2013000837A1 (es) Un sistema de cabrestante para recoger o entregar un cable, comprende un tambor que incluye un cuerpo hueco, un primer y segundo extremo y una red interna, un motor acoplado al primer extremo y que posee un eje de salida; una transmision accionada por el motor e incluye un tren de engranajes planetarios el que incluye un engranaje de entrada y uno de salida; una maquina industrial; y una excavadora minera.
EP2119905A3 (en) Starting and generating apparatus for engine
WO2012112430A3 (en) Regenerative braking safety system and method of use
CL2012001939A1 (es) Método de generación de energía eléctrica, que comprende suministrar de gas presurizado a temperatura y presión dadas; suministrar el gas presurizado a un sistema generador expansor helicoidal de vapor y gas directo (ddg); expandir el gas presurizado; y acoplar el eje de salida a un generador; sistema de generación y uso.
MX373168B (es) Metodo y sistema para generacion de energia auxiliar.
CL2012003223A1 (es) Metodo de posicionamiento de un equipo de perforacion de roca, comprende: impulsar el equipo de perforacion de roca hacia una zona de perforacion, desplazar el equipo con un equipo de impulsion libre de motor de combustion, donde se transmite el movimiento de rotacion del motor de impulsion a traves de una conexion de transmision mecanica antideslizante hacia la rueda de traccion; un equipo de perforacion de roca.
MX2017015642A (es) Sistema de control de generacion de energia para vehículo hibrido.
CO6680682A2 (es) Turbina de tornillo y método de generación de energía
MX2016008503A (es) Aparato de control para vehiculo.
JP2017534014A5 (enExample)
EA201190270A2 (ru) Гибридное транспортное средство
BR112017010895A2 (pt) método e sistema para recuperar e utilizar energia de operação de guindaste, e guindaste
BR112017025943A2 (pt) dispositivo de controle de partida para veículos eletricamente acionados
MX2017012954A (es) Dispositivo de control de cambio de velocidades de vehiculo.
IN2012DN03060A (enExample)