BR112012015746A2 - aeronave incluíndo um gerador de partida elétrica para o ou cada turbojato e um carrinho encaixado com um motor elétrico para realização de taxi - Google Patents

aeronave incluíndo um gerador de partida elétrica para o ou cada turbojato e um carrinho encaixado com um motor elétrico para realização de taxi

Info

Publication number
BR112012015746A2
BR112012015746A2 BR112012015746A BR112012015746A BR112012015746A2 BR 112012015746 A2 BR112012015746 A2 BR 112012015746A2 BR 112012015746 A BR112012015746 A BR 112012015746A BR 112012015746 A BR112012015746 A BR 112012015746A BR 112012015746 A2 BR112012015746 A2 BR 112012015746A2
Authority
BR
Brazil
Prior art keywords
electric
turbojet
starter generator
aircraft including
cart
Prior art date
Application number
BR112012015746A
Other languages
English (en)
Other versions
BR112012015746B1 (pt
Inventor
Didier Francois Marie Godart
Serge Berenger
Original Assignee
Hispano Suiza 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 Hispano Suiza Sa filed Critical Hispano Suiza Sa
Publication of BR112012015746A2 publication Critical patent/BR112012015746A2/pt
Publication of BR112012015746B1 publication Critical patent/BR112012015746B1/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/32—Alighting gear characterised by elements which contact the ground or similar surface 
    • B64C25/405—Powered wheels, e.g. for taxing
    • 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
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • 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
    • B64D31/00—Power plant control systems; Arrangement of power plant control systems in aircraft
    • B64D31/14—Transmitting means between initiating means and power plants
    • 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
    • B64D2221/00—Electric power distribution systems onboard aircraft
    • 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
    • Y02T50/80—Energy efficient operational measures, e.g. ground operations or mission management

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)
  • Control Of Eletrric Generators (AREA)

Abstract

aeronave incluindo um gerador de partida elétrica para o ou cada turbojarto e um carrinho encaixado com um motor elétrico para realização de taxi a mutualização do conversor de eletricidade para dar partida e para taxiar uma aeronave. de acordo com a invenção, um único conversor de eletricidade (14) é adequado para ser acoplado ao gerador de partida elétrica (gd1) associado com um turbojato (m1) ou ao motor elétrico (17) do carrinho de taxi, o acoplamento ocorrendo através de uma unidade de distribuição de eletricidade (12).
BR112012015746-9A 2009-12-23 2010-12-15 aeronave incluindo um gerador de partida elétrica para o ou cada turbojato e um carrinho encaixado com um motor elétrico para realização de taxiamento BR112012015746B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0959540 2009-12-23
FR0959540A FR2954283B1 (fr) 2009-12-23 2009-12-23 Aeronef comportant un demarreur-generateur electrique pour le ou chaque turboreacteur et un train d'aterrissage equipe d'un moteur electrique de manoeuvre au sol
PCT/FR2010/052734 WO2011086258A1 (fr) 2009-12-23 2010-12-15 Aeronef comportant un demarreur-generateur electrique pour le ou chaque turboreacteur et un train d'atterrissage equipe d'un moteur electrique de manoeuvre au sol

Publications (2)

Publication Number Publication Date
BR112012015746A2 true BR112012015746A2 (pt) 2016-05-17
BR112012015746B1 BR112012015746B1 (pt) 2020-07-28

Family

ID=42245994

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112012015746-9A BR112012015746B1 (pt) 2009-12-23 2010-12-15 aeronave incluindo um gerador de partida elétrica para o ou cada turbojato e um carrinho encaixado com um motor elétrico para realização de taxiamento

Country Status (9)

Country Link
US (1) US9227725B2 (pt)
EP (1) EP2516265B1 (pt)
JP (1) JP2013515644A (pt)
CN (1) CN102686479B (pt)
BR (1) BR112012015746B1 (pt)
CA (1) CA2785309C (pt)
FR (1) FR2954283B1 (pt)
RU (1) RU2561522C2 (pt)
WO (1) WO2011086258A1 (pt)

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FR2978878B1 (fr) * 2011-08-04 2013-08-09 Hispano Suiza Sa Dispositif d'alimentation electrique d'un aeronef au sol.
FR2988694B1 (fr) * 2012-03-30 2014-03-28 Hispano Suiza Sa Dispositif d'alimentation electrique d'un aeronef au sol
EP2842873B1 (en) * 2013-08-30 2017-06-14 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Short term, autonomous, electrical power supply system
FR3019218B1 (fr) * 2014-03-27 2016-03-18 Turbomeca Architecture d'un systeme propulsif d'un helicoptere multi-moteur et helicoptere correspondant
US20150283908A1 (en) * 2014-04-02 2015-10-08 Hamilton Sundstrand Corporation Systems utilizing a controllable voltage ac generator system
US9771149B2 (en) 2015-10-30 2017-09-26 Honeywell International Inc. Gate departure system for aircraft
JP6626328B2 (ja) * 2015-12-02 2019-12-25 株式会社Ihi 航空機の電動タキシングシステム
FR3046598B1 (fr) * 2016-01-11 2018-02-02 Liebherr-Aerospace Toulouse Sas Architecture electrique d'un aeronef a plaque de refroidissement
FR3047771A1 (fr) * 2016-02-16 2017-08-18 Airbus Operations Sas Systeme et procede de demarrage des moteurs d'un aeronef bimoteur
JP6969716B2 (ja) * 2019-09-30 2021-11-24 株式会社テクノスヤシマ エンジン始動装置
CN111516887A (zh) * 2020-04-30 2020-08-11 中国商用飞机有限责任公司 自动滑行系统、供电系统、飞行器及供电方法

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US7237748B2 (en) * 2003-12-15 2007-07-03 Delos Aerospace, Llc Landing gear method and apparatus for braking and maneuvering
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FR2900635B1 (fr) * 2006-05-05 2008-07-25 Hispano Suiza Sa Systeme d'alimentation et de commande d'equipements electriques d'un moteur d'aeronef ou de son environnement
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Also Published As

Publication number Publication date
EP2516265A1 (fr) 2012-10-31
US20130048781A1 (en) 2013-02-28
US9227725B2 (en) 2016-01-05
CA2785309A1 (fr) 2011-07-21
CN102686479B (zh) 2016-09-07
FR2954283A1 (fr) 2011-06-24
JP2013515644A (ja) 2013-05-09
RU2561522C2 (ru) 2015-08-27
CN102686479A (zh) 2012-09-19
FR2954283B1 (fr) 2012-03-02
WO2011086258A1 (fr) 2011-07-21
CA2785309C (fr) 2017-11-07
EP2516265B1 (fr) 2014-07-02
BR112012015746B1 (pt) 2020-07-28
RU2012131175A (ru) 2014-01-27

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according art. 34 industrial property law
B06U Preliminary requirement: requests with searches performed by other patent offices: suspension of the patent application procedure
B09A Decision: intention to grant
B16A Patent or certificate of addition of invention granted

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 15/12/2010, OBSERVADAS AS CONDICOES LEGAIS.