BRPI0700685A - arquitetura de distribuição de potência elétrica adaptada especialmente para atuar em seqüência elementos móveis de aeronave - Google Patents

arquitetura de distribuição de potência elétrica adaptada especialmente para atuar em seqüência elementos móveis de aeronave

Info

Publication number
BRPI0700685A
BRPI0700685A BRPI0700685-3A BRPI0700685A BRPI0700685A BR PI0700685 A BRPI0700685 A BR PI0700685A BR PI0700685 A BRPI0700685 A BR PI0700685A BR PI0700685 A BRPI0700685 A BR PI0700685A
Authority
BR
Brazil
Prior art keywords
power distribution
elements
electrical power
aircraft
electric power
Prior art date
Application number
BRPI0700685-3A
Other languages
English (en)
Inventor
Jean-Pierre Garcia
Original Assignee
Messier Bugatti
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 Messier Bugatti filed Critical Messier Bugatti
Publication of BRPI0700685A publication Critical patent/BRPI0700685A/pt
Publication of BRPI0700685B1 publication Critical patent/BRPI0700685B1/pt

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C25/00Alighting gear
    • B64C25/02Undercarriages
    • B64C25/08Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/18Operating mechanisms
    • B64C25/24Operating mechanisms electric
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • B64C9/14Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • B64C9/14Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/22Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JELECTRIC POWER NETWORKS; CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J4/00Circuit arrangements for mains or distribution networks not specified as AC or DC; Circuit arrangements for mains or distribution networks combining AC and DC sections or sub-networks
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D2221/00Electric power distribution systems onboard aircraft
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02JELECTRIC POWER NETWORKS; CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J2105/00Networks for supplying or distributing electric power characterised by their spatial reach or by the load
    • H02J2105/30Networks for supplying or distributing electric power characterised by their spatial reach or by the load the load networks being external to vehicles, i.e. exchanging power with vehicles
    • H02J2105/32Networks for supplying or distributing electric power characterised by their spatial reach or by the load the load networks being external to vehicles, i.e. exchanging power with vehicles for aircrafts
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Power Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Transmission Devices (AREA)
  • Retarders (AREA)
  • Direct Current Feeding And Distribution (AREA)
  • Current-Collector Devices For Electrically Propelled Vehicles (AREA)
  • Stand-By Power Supply Arrangements (AREA)

Abstract

ARQUITETURA DE DISTRIBUIçãO DE POTêNCIA ELéTRICA ADAPTADA ESPECIALMENTE PARA ATUAR EM SEQüêNCIA ELEMENTOS MóVEIS DE AERONAVE A invenção relaciona-se a uma arquitetura de distribuição de potência elétrica adaptada especialmente para atuar em seqüência elementos móveis de aeronave tais como portas, trens de pouso, ou elementos de alta sustentação, ditos elementos móveis sendo atuados por amadores eletromecânicos energizados em seqüência de potência elétrica entregue por pelo menos um barramento de potência elétrica da aeronave. De acordo com a invenção, a arquitetura inclui pelo menos um membro de distribuição de potência (710, 720, ..., 760) incluindo: meio de calibrador (711, 721, ..., 761) para calibrar a potência elétrica vindo do barramento de provisão de potência da aeronave; e meio de chave (712, 722, ..., 762) para dirigir seletivamente a potência elétrica calibrada para um ou o outro dos amadores eletromecânicos.
BRPI0700685-3A 2006-03-13 2007-03-13 Arquitetura de distribuição de energia elétrica adaptada especialmente para atuar em seqüência elementos móveis de aeronave BRPI0700685B1 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0602180 2006-03-13
FR0602180A FR2898337B1 (fr) 2006-03-13 2006-03-13 Architecture de distribution de puissance pour actionnements en sequence d'elements mobiles d'un aeronef

Publications (2)

Publication Number Publication Date
BRPI0700685A true BRPI0700685A (pt) 2007-11-06
BRPI0700685B1 BRPI0700685B1 (pt) 2018-03-20

Family

ID=37308866

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0700685-3A BRPI0700685B1 (pt) 2006-03-13 2007-03-13 Arquitetura de distribuição de energia elétrica adaptada especialmente para atuar em seqüência elementos móveis de aeronave

Country Status (10)

Country Link
US (1) US7786615B2 (pt)
EP (1) EP1834874B1 (pt)
JP (1) JP4564024B2 (pt)
CN (1) CN101039033B (pt)
AT (1) ATE480453T1 (pt)
BR (1) BRPI0700685B1 (pt)
CA (1) CA2581399C (pt)
DE (1) DE602007008967D1 (pt)
ES (1) ES2351475T3 (pt)
FR (1) FR2898337B1 (pt)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2940245B1 (fr) 2008-12-22 2011-03-18 Messier Bugatti Architecture de distribution de puissance pour distribuer la puissance a des actionneurs electromecaniques d'un aeronef
FR2961479B1 (fr) 2010-06-18 2014-01-17 Sagem Defense Securite Aeronef pourvu d'une pluralite d'actionneurs electriques, dispositif d'alimentation et de commande de tels actionneurs et ensemble d'actionnement correspondant
FR2980461B1 (fr) * 2011-09-26 2013-10-04 Messier Bugatti Dowty Dispositif de manoeuvre au sol d'une trappe d'un atterrisseur d'aeronef.
CN105346707B (zh) * 2015-12-02 2023-08-15 上海航空电器有限公司 一种具有昼夜转换指示功能的起落架操纵开关
US10994862B2 (en) * 2017-08-02 2021-05-04 Airbus Operations Sas Modular element for an electrical power distribution network of an aircraft
US11066153B2 (en) * 2019-09-20 2021-07-20 Goodrich Corporation Electric nose landing gear architecture
BR102021003968A2 (pt) * 2020-03-05 2021-09-14 Goodrich Corporation Sistema de trem de pouso, e, sistema para controlar subsistemas de trem de pouso
US11472539B2 (en) * 2020-03-05 2022-10-18 Goodrich Corporation Distributed landing gear system architecture for electromechanical actuation

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5594285A (en) * 1993-08-27 1997-01-14 Sundstrand Corporation Power distribution center
US5850113A (en) * 1997-04-15 1998-12-15 The United States Of America As Represented By The Secretary Of The Air Force Super capacitor battery clone
GB9926354D0 (en) * 1999-11-08 2000-01-12 Rolls Royce Plc Power supply system for an aircraft
US20030020330A1 (en) * 2001-07-12 2003-01-30 Cratty William E. DC ladder bus

Also Published As

Publication number Publication date
JP4564024B2 (ja) 2010-10-20
FR2898337B1 (fr) 2009-02-13
CA2581399A1 (fr) 2007-09-13
US20070262643A1 (en) 2007-11-15
DE602007008967D1 (de) 2010-10-21
CN101039033A (zh) 2007-09-19
EP1834874A1 (fr) 2007-09-19
CA2581399C (fr) 2010-05-11
ES2351475T3 (es) 2011-02-07
ATE480453T1 (de) 2010-09-15
CN101039033B (zh) 2011-03-23
BRPI0700685B1 (pt) 2018-03-20
EP1834874B1 (fr) 2010-09-08
JP2007246083A (ja) 2007-09-27
US7786615B2 (en) 2010-08-31
FR2898337A1 (fr) 2007-09-14

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Legal Events

Date Code Title Description
B25D Requested change of name of applicant approved

Owner name: MESSIER-BUGATTI-DOWTY (FR)

Free format text: NOME ALTERADO DE: MESSIER-BUGATTI

B25G Requested change of headquarter approved

Owner name: MESSIER-BUGATTI-DOWTY (FR)

Free format text: ENDERECO ALTERADO CONFORME SOLICITADO NA PETICAO NO 020120020080/RJ DE 09/03/2012.

B06A Patent application procedure suspended [chapter 6.1 patent gazette]
B15K Others concerning applications: alteration of classification

Ipc: H02J 4/00 (1974.07), B64D 41/00 (1968.09), B64C 25

B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]
B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time

Free format text: REFERENTE A 17A ANUIDADE.

B24J Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12)

Free format text: EM VIRTUDE DA EXTINCAO PUBLICADA NA RPI 2766 DE 09-01-2024 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDA A EXTINCAO DA PATENTE E SEUS CERTIFICADOS, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.