BR112016005119A2 - sistema e método de arranque de emergência de uma turbomáquina de aeronave - Google Patents

sistema e método de arranque de emergência de uma turbomáquina de aeronave

Info

Publication number
BR112016005119A2
BR112016005119A2 BR112016005119A BR112016005119A BR112016005119A2 BR 112016005119 A2 BR112016005119 A2 BR 112016005119A2 BR 112016005119 A BR112016005119 A BR 112016005119A BR 112016005119 A BR112016005119 A BR 112016005119A BR 112016005119 A2 BR112016005119 A2 BR 112016005119A2
Authority
BR
Brazil
Prior art keywords
emergency start
start method
aircraft turbomachine
igniter
generator
Prior art date
Application number
BR112016005119A
Other languages
English (en)
Other versions
BR112016005119B1 (pt
Inventor
Marie Georges Caratge Antoine
Serghine Camel
Danguy François
Fabbri Laurent
Soulie Laurent
Marconi Patrick
Barrat Philippe
Yvart Pierre
Thiriet Romain
Original Assignee
1 Snecma 2 Turbomeca E 3 Herakles
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 1 Snecma 2 Turbomeca E 3 Herakles filed Critical 1 Snecma 2 Turbomeca E 3 Herakles
Publication of BR112016005119A2 publication Critical patent/BR112016005119A2/pt
Publication of BR112016005119B1 publication Critical patent/BR112016005119B1/pt

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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D19/00—Starting of machines or engines; Regulating, controlling, or safety means in connection therewith
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/20—Adaptations of gas-turbine plants for driving vehicles
    • F02C6/206—Adaptations of gas-turbine plants for driving vehicles the vehicles being airscrew driven
    • 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
    • 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
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Turbines (AREA)
  • Supercharger (AREA)

Abstract

sistema (20) de arranque de emergência de uma turbo-máquina de aeronave, caracterizado pelo fato de que inclui pelo menos um gerador de gás (22) a propelente sólido, um dispositivo de ignição (24) acionado eletricamente, um computador (28) ligado ao dispositivo de ignição, e ao menos um motor de arranque (18) que inclui uma turbina (38) de acionamento de um eixo (34) destinado a ser acoplado a um eixo (54) da turbo-máquina, a saída de gás do gerador sendo ligada à entrada (44) da turbina do motor de arranque.
BR112016005119-0A 2013-09-19 2014-09-12 Sistema de arranque de emergência de turbo-máquinas de aeronave, aeronave e método de arranque de emergência de uma turbo-máquina de aeronave BR112016005119B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1358996 2013-09-19
FR1358996A FR3010740B1 (fr) 2013-09-19 2013-09-19 Systeme et procede de demarrage d'urgence d'une turbomachine d'aeronef
PCT/FR2014/052263 WO2015040310A1 (fr) 2013-09-19 2014-09-12 Système et procédé de démarrage d'urgence d'une turbomachine d'aéronef

Publications (2)

Publication Number Publication Date
BR112016005119A2 true BR112016005119A2 (pt) 2018-03-20
BR112016005119B1 BR112016005119B1 (pt) 2021-11-30

Family

ID=50097787

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112016005119-0A BR112016005119B1 (pt) 2013-09-19 2014-09-12 Sistema de arranque de emergência de turbo-máquinas de aeronave, aeronave e método de arranque de emergência de uma turbo-máquina de aeronave

Country Status (12)

Country Link
US (1) US9951694B2 (pt)
EP (1) EP3047117B1 (pt)
JP (1) JP6454714B2 (pt)
KR (1) KR102242938B1 (pt)
CN (1) CN105658915B (pt)
BR (1) BR112016005119B1 (pt)
CA (1) CA2922989C (pt)
ES (1) ES2649552T3 (pt)
FR (1) FR3010740B1 (pt)
PL (1) PL3047117T3 (pt)
RU (1) RU2660725C2 (pt)
WO (1) WO2015040310A1 (pt)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3024180B1 (fr) * 2014-07-28 2016-07-22 Turbomeca Dispositif pneumatique de reactivation rapide d'un turbomoteur, architecture d'un systeme propulsif d'un helicoptere multi-moteur equipe d'un tel dispositif et helicoptere correspondant
FR3050815B1 (fr) * 2016-04-28 2019-05-24 Safran Helicopter Engines Systeme d'allumage et dispositif d'entrainement mecanique associe
US10371002B2 (en) * 2016-06-14 2019-08-06 General Electric Company Control system for a gas turbine engine
CN106481457B (zh) * 2016-10-28 2017-11-24 西安近代化学研究所 一种固体燃气启动器
CN110939529B (zh) * 2019-11-25 2020-11-06 西安航天动力研究所 一种集成式燃气供应装置
US11794914B2 (en) 2021-07-19 2023-10-24 Pratt & Whitney Canada Corp. Emergency power unit for electric aircraft

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB885542A (en) * 1957-05-29 1961-12-28 Garrett Corp Improvements relating to engine starting systems
FR1361269A (fr) * 1962-07-02 1964-05-15 Garrett Corp Turbine
FR1448767A (fr) * 1964-10-08 1966-03-18 Sundstrand A G Distributeur de commande de vitesse de combustion pour un démarreur à cartouche, notamment pour turbo-réacteur
GB1103417A (en) * 1965-12-07 1968-02-14 Dowty Rotol Ltd Engine installations and starting means therefor
US4542722A (en) * 1983-12-19 1985-09-24 Sundstrand Corporation Combined engine-starter and accessory drive system
DE3502578A1 (de) * 1985-01-26 1986-07-31 Klöckner-Humboldt-Deutz AG, 5000 Köln Hilfsantrieb fuer ein gasturbinentriebwerk
US5069692A (en) * 1989-12-11 1991-12-03 Sundstrand Corporation Fully integrated inert gas and oxidizer replenishment system
RU2005898C1 (ru) * 1992-04-15 1994-01-15 Моторостроительное конструкторское бюро Способ аварийного обеспечения энергией вспомогательной силовой установки систем жизнеобеспечения самолета
RU2224690C2 (ru) * 2000-12-20 2004-02-27 Федеральное государственное унитарное предприятие Российская самолетостроительная корпорация "МиГ" Силовая установка летательного аппарата
US6993915B2 (en) * 2004-02-26 2006-02-07 Honeywell International Inc. Solid propellant gas generators in power systems
FR2929324B1 (fr) * 2008-03-25 2012-10-12 Turbomeca Turbomoteur comportant une machine electrique reversible
US20100326085A1 (en) * 2009-06-25 2010-12-30 Veilleux Leo J Lightweight start system for a gas turbine engine
FR2967132B1 (fr) * 2010-11-04 2012-11-09 Turbomeca Procede d'optimisation de la consommation specifique d'un helicoptere bimoteur et architecture bimoteur dissymetrique a systeme de regulation pour sa mise en oeuvre

Also Published As

Publication number Publication date
KR20160057401A (ko) 2016-05-23
KR102242938B1 (ko) 2021-04-20
CA2922989C (fr) 2021-02-23
US20160230672A1 (en) 2016-08-11
RU2016109790A3 (pt) 2018-05-22
CN105658915B (zh) 2018-08-28
EP3047117B1 (fr) 2017-11-01
FR3010740A1 (fr) 2015-03-20
FR3010740B1 (fr) 2018-03-02
RU2660725C2 (ru) 2018-07-09
CA2922989A1 (fr) 2015-03-26
RU2016109790A (ru) 2017-10-24
JP2016532057A (ja) 2016-10-13
CN105658915A (zh) 2016-06-08
BR112016005119B1 (pt) 2021-11-30
WO2015040310A1 (fr) 2015-03-26
US9951694B2 (en) 2018-04-24
EP3047117A1 (fr) 2016-07-27
JP6454714B2 (ja) 2019-01-16
ES2649552T3 (es) 2018-01-12
PL3047117T3 (pl) 2018-02-28

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Legal Events

Date Code Title Description
B25F Entry of change of name and/or headquarter and transfer of application, patent and certif. of addition of invention: change of name on requirement

Owner name: 1) SNECMA; 2) TURBOMECA; E 3) HERAKLES (FR)

B25D Requested change of name of applicant approved

Owner name: SAFRAN AIRCRAFT ENGINES (FR) ; TURBOMECA (FR) ; HE

B25D Requested change of name of applicant approved

Owner name: SAFRAN AIRCRAFT ENGINES (FR) ; HERAKLES (FR) ; SAFRAN HELICOPTER ENGINES (FR)

Owner name: SAFRAN AIRCRAFT ENGINES (FR) ; HERAKLES (FR) ; SAF

B25D Requested change of name of applicant approved

Owner name: SAFRAN AIRCRAFT ENGINES (FR) ; SAFRAN HELICOPTER E

B25A Requested transfer of rights approved

Owner name: SAFRAN AIRCRAFT ENGINES (FR) ; SAFRAN HELICOPTER E

B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 12/09/2014, OBSERVADAS AS CONDICOES LEGAIS.