BRPI0704042A - arquitetura para um sistema hidráulico - Google Patents

arquitetura para um sistema hidráulico

Info

Publication number
BRPI0704042A
BRPI0704042A BRPI0704042-3A BRPI0704042A BRPI0704042A BR PI0704042 A BRPI0704042 A BR PI0704042A BR PI0704042 A BRPI0704042 A BR PI0704042A BR PI0704042 A BRPI0704042 A BR PI0704042A
Authority
BR
Brazil
Prior art keywords
line
hydraulic
architecture
return
selector
Prior art date
Application number
BRPI0704042-3A
Other languages
English (en)
Inventor
David Leutard
Eric Felemez
Sebastien Fremiot
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 BRPI0704042A publication Critical patent/BRPI0704042A/pt
Publication of BRPI0704042B1 publication Critical patent/BRPI0704042B1/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C25/00—Alighting gear
    • B64C25/02—Undercarriages
    • B64C25/08—Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10—Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/18—Operating mechanisms
    • B64C25/22—Operating mechanisms fluid
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B20/00—Safety arrangements for fluid actuator systems; Applications of safety devices in fluid actuator systems; Emergency measures for fluid actuator systems
    • F15B20/004—Fluid pressure supply failure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B20/00—Safety arrangements for fluid actuator systems; Applications of safety devices in fluid actuator systems; Emergency measures for fluid actuator systems
    • F15B20/008—Valve failure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B2211/00—Circuits for servomotor systems
    • F15B2211/60—Circuit components or control therefor
    • F15B2211/63—Electronic controllers
    • F15B2211/6303—Electronic controllers using input signals
    • F15B2211/6306—Electronic controllers using input signals representing a pressure
    • F15B2211/6309—Electronic controllers using input signals representing a pressure the pressure being a pressure source supply pressure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B2211/00—Circuits for servomotor systems
    • F15B2211/70—Output members, e.g. hydraulic motors or cylinders or control therefor
    • F15B2211/705—Output members, e.g. hydraulic motors or cylinders or control therefor characterised by the type of output members or actuators
    • F15B2211/7051—Linear output members
    • F15B2211/7053—Double-acting output members
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B2211/00—Circuits for servomotor systems
    • F15B2211/70—Output members, e.g. hydraulic motors or cylinders or control therefor
    • F15B2211/71—Multiple output members, e.g. multiple hydraulic motors or cylinders
    • F15B2211/7114—Multiple output members, e.g. multiple hydraulic motors or cylinders with direct connection between the chambers of different actuators
    • F15B2211/7128—Multiple output members, e.g. multiple hydraulic motors or cylinders with direct connection between the chambers of different actuators the chambers being connected in parallel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B2211/00—Circuits for servomotor systems
    • F15B2211/80—Other types of control related to particular problems or conditions
    • F15B2211/86—Control during or prevention of abnormal conditions
    • F15B2211/863—Control during or prevention of abnormal conditions the abnormal condition being a hydraulic or pneumatic failure
    • F15B2211/8633—Pressure source supply failure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B2211/00—Circuits for servomotor systems
    • F15B2211/80—Other types of control related to particular problems or conditions
    • F15B2211/86—Control during or prevention of abnormal conditions
    • F15B2211/863—Control during or prevention of abnormal conditions the abnormal condition being a hydraulic or pneumatic failure
    • F15B2211/8636—Circuit failure, e.g. valve or hose failure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
    • F15B—SYSTEMS ACTING BY MEANS OF FLUIDS IN GENERAL; FLUID-PRESSURE ACTUATORS, e.g. SERVOMOTORS; DETAILS OF FLUID-PRESSURE SYSTEMS, NOT OTHERWISE PROVIDED FOR
    • F15B2211/00—Circuits for servomotor systems
    • F15B2211/80—Other types of control related to particular problems or conditions
    • F15B2211/875—Control measures for coping with failures
    • F15B2211/8752—Emergency operation mode, e.g. fail-safe operation mode

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Analytical Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fluid-Pressure Circuits (AREA)

Abstract

ARQUITETURA PARA UM SISTEMA HIDRáULICO. A invenção diz respeito a uma arquitetura para um sistema hidráulico para operar o trem de pouso de uma aeronave incluindo pelo menos uma fonte de pressão e pelo menos um retorno hidráulico, o sistema tendo um circuito hidráulico que compreende uma primeira linha hidráulica ("DOWN") que, quando pressurizada, faz com que o trem de pouso seja abaixado, e uma segunda linha hidráulica ("UP" 5) que, quando pressurizada, faz com que o trem de pouso seja recolhido, as ditas linhas sendo seletivamente pressurizadas por meio de um elemento de distribuição hidráulico (10, 12) compreendendo pelo menos uma válvula de isolamento (10) e um seletor (12) para colocar uma das linhas em comunicação com pressão e a outra linha em comunicação com o retorno. De acordo com a invenção, a arquitetura inclui meio de desvio passivo (54, 55) para desviar do seletor, o dito meio sendo disposto entre a segunda linha ("UP" 5) e uma linha de admissão (20) que estende-se entre a válvula de isolamento e o seletor, e meio de conexão de retorno forçado (53) para forçar a válvula de isolamento (10) isolar o circuito de pressão da aeronave e conectar a linha de admissão no retorno.
BRPI0704042A 2006-10-17 2007-10-16 arquitetura para um sistema hidráulico BRPI0704042B1 (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0609093A FR2907097B1 (fr) 2006-10-17 2006-10-17 Architecture de systeme hydraulique de manoeuvre d'atterrisseurs d'aeronef

Publications (2)

Publication Number Publication Date
BRPI0704042A true BRPI0704042A (pt) 2008-06-03
BRPI0704042B1 BRPI0704042B1 (pt) 2018-12-04

Family

ID=38051002

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0704042A BRPI0704042B1 (pt) 2006-10-17 2007-10-16 arquitetura para um sistema hidráulico

Country Status (8)

Country Link
US (1) US8028954B2 (pt)
EP (1) EP1914163B1 (pt)
JP (1) JP4763672B2 (pt)
CN (1) CN100588592C (pt)
BR (1) BRPI0704042B1 (pt)
CA (1) CA2606726C (pt)
ES (1) ES2388934T3 (pt)
FR (1) FR2907097B1 (pt)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2933670B1 (fr) * 2008-07-08 2011-04-08 Airbus France Systeme d'ouverture et de fermeture de trappe pour case de train d'atterrissage d'un aeronef
GB2469484B (en) * 2009-04-15 2013-09-18 Ge Aviat Systems Ltd Landing gear actuation control system
DE102010014340B4 (de) 2010-04-09 2013-02-21 Airbus Operations Gmbh Schutzvorrichtung für eine Druckleitung und Druckleitungsabschnitt
FR2966428B1 (fr) * 2010-10-20 2013-08-02 Messier Bugatti Circuit hydraulique d'actionnement d'un atterrisseur et procedes de deploiement et de relevage d'un atterrisseur utilisant un tel circuit.
FR2982240B1 (fr) 2011-11-09 2013-12-13 Messier Bugatti Dowty Procede de deploiement d'atterrisseurs d'aeronef en mode secours.
CN104369860B (zh) * 2014-11-27 2016-08-24 江西洪都航空工业集团有限责任公司 一种集成式起落架收放优先控制开关
CN105151282A (zh) * 2015-09-14 2015-12-16 江西洪都航空工业集团有限责任公司 一种飞机起落架地面可靠上锁的控制方法
US10150558B2 (en) 2016-06-30 2018-12-11 DZYNE Technologies Incorporated Tilting landing gear systems and methods
US11433991B2 (en) * 2018-12-31 2022-09-06 Blended Wing Aircraft, Inc. Tilting landing gear systems and methods
US12304620B2 (en) * 2016-06-30 2025-05-20 Jetzero, Inc. Tilting landing gear systems and methods
US11453483B2 (en) 2016-06-30 2022-09-27 Blended Wing Aircraft, Inc. Aircraft for commercial air travel and a method of manufacture
CN108167242B (zh) * 2016-12-07 2019-08-20 中国航空工业集团公司成都飞机设计研究所 一种高压流体驱动系统
CN106697266A (zh) * 2016-12-28 2017-05-24 中国航空工业集团公司西安飞机设计研究所 一种飞机起落架收放控制系统
FR3088898B1 (fr) * 2018-11-23 2020-12-18 Safran Landing Systems Circuit hydraulique de manœuvre de train d’atterrissage d’aéronef
CN109515696B (zh) * 2018-12-29 2023-10-31 南通华夏飞机工程技术股份有限公司 一种飞机起落架收放液压系统
FR3106633B1 (fr) * 2020-01-24 2022-02-04 Safran Landing Systems Actionneur à port d’alimentation déporté
FR3111620B1 (fr) * 2020-06-23 2022-07-01 Safran Landing Systems Dispositif de verrouillage d’atterrisseur
CN112339995B (zh) * 2020-10-29 2022-01-11 中电科芜湖通用航空产业技术研究院有限公司 一种液压收放起落架机构

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2459665A (en) * 1944-12-26 1949-01-18 Warner Aircraft Corp Combined retracting and braking system for aircraft landing gear
GB757705A (en) * 1953-04-02 1956-09-26 Electro Hydraulics Ltd Fluid pressure operated systems
GB973364A (en) * 1961-10-11 1964-10-28 Dowty Rotol Ltd Fluid-pressure-operated-systems
US3173630A (en) * 1961-11-07 1965-03-16 Jerome L Milana Aircraft landing gear emergency hydraulic system
FR2684066B1 (fr) * 1991-11-26 1994-01-07 Messier Bugatti Systeme d'actionnement du verin de manóoeuvre d'un train d'atterrissage d'avion.
JP3671198B2 (ja) * 1997-06-13 2005-07-13 ナブテスコ株式会社 航空機用脚昇降装置
GB9923620D0 (en) * 1999-10-07 1999-12-08 Normalair Garrett Ltd Hydraulic system for aircraft landing gear
JP3940645B2 (ja) * 2002-07-16 2007-07-04 カヤバ工業株式会社 航空機用降着装置

Also Published As

Publication number Publication date
CA2606726A1 (fr) 2008-04-17
FR2907097B1 (fr) 2009-01-16
ES2388934T3 (es) 2012-10-19
JP4763672B2 (ja) 2011-08-31
CN100588592C (zh) 2010-02-10
BRPI0704042B1 (pt) 2018-12-04
JP2008132970A (ja) 2008-06-12
EP1914163A1 (fr) 2008-04-23
EP1914163B1 (fr) 2012-07-18
CN101172521A (zh) 2008-05-07
US8028954B2 (en) 2011-10-04
FR2907097A1 (fr) 2008-04-18
CA2606726C (fr) 2010-07-13
US20080087765A1 (en) 2008-04-17

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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 020120019935/RJ DE 09/03/2012.

B07A Application suspended after technical examination (opinion) [chapter 7.1 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: 10 (DEZ) ANOS CONTADOS A PARTIR DE 04/12/2018, OBSERVADAS AS CONDICOES LEGAIS.

B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time

Free format text: REFERENTE A 16A 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 2744 DE 08-08-2023 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.