BRPI0915777A2 - sistema de trem de pouso, atuador de trem de pouso, e, método para ciclar um trem de pouso entre posições recolhida e estendida - Google Patents

sistema de trem de pouso, atuador de trem de pouso, e, método para ciclar um trem de pouso entre posições recolhida e estendida

Info

Publication number
BRPI0915777A2
BRPI0915777A2 BRPI0915777A BRPI0915777A BRPI0915777A2 BR PI0915777 A2 BRPI0915777 A2 BR PI0915777A2 BR PI0915777 A BRPI0915777 A BR PI0915777A BR PI0915777 A BRPI0915777 A BR PI0915777A BR PI0915777 A2 BRPI0915777 A2 BR PI0915777A2
Authority
BR
Brazil
Prior art keywords
landing gear
main
emergency
actuator
drive
Prior art date
Application number
BRPI0915777A
Other languages
English (en)
Inventor
Andrew John Collins
Original Assignee
Hamilton Sundstrand Corp
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 Hamilton Sundstrand Corp filed Critical Hamilton Sundstrand Corp
Publication of BRPI0915777A2 publication Critical patent/BRPI0915777A2/pt
Publication of BRPI0915777B1 publication Critical patent/BRPI0915777B1/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
    • B64C25/00Alighting gear
    • B64C25/02Undercarriages
    • B64C25/08Undercarriages non-fixed, e.g. jettisonable
    • B64C25/10Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like
    • B64C25/12Undercarriages non-fixed, e.g. jettisonable retractable, foldable, or the like sideways
    • 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
    • B64C25/26Control or locking systems therefor
    • B64C25/30Control or locking systems therefor emergency actuated
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K7/00Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/06Means for converting reciprocating motion into rotary motion or vice versa
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H25/00Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms
    • F16H25/18Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms for conveying or interconverting oscillating or reciprocating motions
    • F16H25/20Screw mechanisms
    • F16H2025/2062Arrangements for driving the actuator
    • F16H2025/2071Disconnecting drive source from the actuator, e.g. using clutches for release of drive connection during manual control
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H25/00Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms
    • F16H25/18Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms for conveying or interconverting oscillating or reciprocating motions
    • F16H25/20Screw mechanisms
    • F16H2025/2062Arrangements for driving the actuator
    • F16H2025/2081Parallel arrangement of drive motor to screw axis
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H25/00Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms
    • F16H25/18Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms for conveying or interconverting oscillating or reciprocating motions
    • F16H25/20Screw mechanisms
    • F16H25/205Screw mechanisms comprising alternate power paths, e.g. for fail safe back-up
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16HGEARING
    • F16H25/00Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms
    • F16H25/18Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms for conveying or interconverting oscillating or reciprocating motions
    • F16H25/20Screw mechanisms
    • F16H25/24Elements essential to such mechanisms, e.g. screws, nuts
    • F16H25/2454Brakes; Rotational locks

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Power Engineering (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Transmission Devices (AREA)
  • Braking Arrangements (AREA)
  • Gear Transmission (AREA)
  • Retarders (AREA)
  • Body Structure For Vehicles (AREA)
  • Elevator Door Apparatuses (AREA)
BRPI0915777A 2008-07-16 2009-07-16 sistema de trem de pouso, atuador de trem de pouso, e, método para ciclar um trem de pouso entre posições recolhida e estendida BRPI0915777B1 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/174,038 US8070094B2 (en) 2008-07-16 2008-07-16 Aircraft landing gear actuator
PCT/US2009/050796 WO2010009289A2 (en) 2008-07-16 2009-07-16 Aircraft landing gear actuator

Publications (2)

Publication Number Publication Date
BRPI0915777A2 true BRPI0915777A2 (pt) 2015-11-10
BRPI0915777B1 BRPI0915777B1 (pt) 2019-12-17

Family

ID=41529439

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0915777A BRPI0915777B1 (pt) 2008-07-16 2009-07-16 sistema de trem de pouso, atuador de trem de pouso, e, método para ciclar um trem de pouso entre posições recolhida e estendida

Country Status (8)

Country Link
US (1) US8070094B2 (pt)
EP (1) EP2318272B1 (pt)
KR (1) KR101279354B1 (pt)
CN (1) CN102099248B (pt)
AT (1) ATE548259T1 (pt)
BR (1) BRPI0915777B1 (pt)
CA (1) CA2730926C (pt)
WO (1) WO2010009289A2 (pt)

Families Citing this family (60)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0616730D0 (en) * 2006-08-23 2006-10-04 Airbus Uk Ltd Jam-tolerant actuator
WO2009146148A2 (en) * 2008-04-04 2009-12-03 Tactair Fluid Controls, Inc. Locking mechanism with bi-modal actuator
GB0900815D0 (en) * 2009-01-20 2009-03-04 Airbus Uk Ltd A nose landing gear arrangement for an aircraft and an aircraft having such an arrangement
GB0914576D0 (en) * 2009-08-20 2009-09-30 Airbus Operations Ltd Apparatus for use on an aircraft
FR2951330B1 (fr) * 2009-10-13 2013-03-08 Messier Bugatti Reseau de pilotage pour actionneurs mono ou multimoteurs, particulierement adapte a des applications aeronautiques telles que l'alimentation de moteurs de boitiers d'accrochage
US8590835B2 (en) * 2010-05-11 2013-11-26 Goodrich Corporation Electrically powered downlock actuation system
CN101850844B (zh) * 2010-05-24 2013-04-10 南京航空航天大学 一种飞机起落架
FR2979899B1 (fr) * 2011-09-09 2014-07-18 Messier Bugatti Dowty Dispositif d'attelage d'un actionneur de manœuvre d'un atterrisseur d'aeronef
FR2980461B1 (fr) * 2011-09-26 2013-10-04 Messier Bugatti Dowty Dispositif de manoeuvre au sol d'une trappe d'un atterrisseur d'aeronef.
FR2984276B1 (fr) * 2011-12-15 2014-03-07 Messier Bugatti Dowty Procede de gestion de systemes lies au train d'atterrissage d'un aeronef.
GB2498208B (en) 2012-01-06 2017-12-20 Ge Aviat Systems Ltd Electrical actuator incorporating a free play mechanism to eliminate force fighting
GB2495999B (en) * 2012-02-24 2013-11-13 Messier Dowty Ltd Landing gear
US8899516B2 (en) 2012-04-05 2014-12-02 JHamilton Sundstrand Corporation Coaxial contra-rotating motors for differential landing gear steering
US8973866B2 (en) 2012-04-10 2015-03-10 Hamilton Sundstrand Corporation Transverse flux machine utilized as part of a combined landing gear system
DE102012009106A1 (de) * 2012-04-27 2013-10-31 Liebherr-Aerospace Lindenberg Gmbh Aktuator für ein Fahrwerk eines Luftfahrzeuges
GB2501906A (en) * 2012-05-10 2013-11-13 Ge Aviat Systems Ltd Aircraft landing gear
US9511875B2 (en) 2012-06-06 2016-12-06 Hamilton Sundstrand Corporation Electromechanical actuator damping arrangement for ram air turbine
US9365295B2 (en) 2012-06-06 2016-06-14 Hamilton Sundstrand Corporation Electromechanical actuator and latch assembly for ram air turbine
US9193472B2 (en) 2012-06-06 2015-11-24 Hamilton Sundstrand Corporation Electromechanical actuator lubrication system for ram air turbine
US9383228B2 (en) 2012-12-03 2016-07-05 Hamilton Sundstrand Corporation Control voltage signal synthesis system and method
US20150069178A1 (en) * 2013-09-09 2015-03-12 The Boeing Company Fuselage-mounted landing gear assembly for use with a low wing aircraft
US10214283B2 (en) 2013-09-12 2019-02-26 E.B. Robinson Ltd. Aircraft landing gear and method
GB2518605B (en) * 2013-09-18 2020-02-12 Airbus Operations Ltd Drive system for landing gear
KR101462810B1 (ko) 2013-10-28 2014-11-20 현대위아 주식회사 항공기용 착륙장치
FR3016094B1 (fr) * 2013-12-26 2016-01-22 Tech Pour L En Atomique Soc Actionneur comportant un moteur synchrone a redondances statoriques
CN103754357A (zh) * 2014-01-10 2014-04-30 江苏艾锐泰克无人飞行器科技有限公司 起落架横管及应用该起落架横管的起落架
CN103754355A (zh) * 2014-01-10 2014-04-30 江苏艾锐泰克无人飞行器科技有限公司 收放起落架及无人飞行器
EP2902315A1 (en) * 2014-02-04 2015-08-05 General Atomics Aeronautical Systems, Inc. Landing gear deployment systems and methods
US9399522B2 (en) 2014-02-20 2016-07-26 Hamilton Sundstrand Corporation Ram air turbine actuator
US9797490B2 (en) 2014-03-27 2017-10-24 Lcdrives Corp. High reliability actuator
KR101651085B1 (ko) 2014-08-26 2016-09-05 알파비젼(주) 열가소성 플라스틱 조명반사체 및 그 제조방법과 성형몰드구조
CN104190088A (zh) * 2014-09-19 2014-12-10 安徽工程大学 一种航模直升机起落架
EP3020632B1 (en) * 2014-11-13 2018-12-26 Safran Landing Systems UK Limited Aircraft landing gear assembly
CN104743101B (zh) * 2015-03-30 2016-08-17 中国民用航空飞行学院 通航飞机起落架收放系统
CN112722300A (zh) * 2015-04-21 2021-04-30 高途乐公司 空中捕获平台
EP3135581B1 (en) * 2015-08-25 2018-03-21 Safran Landing Systems UK Limited Aircraft landing gear assembly
CN106838186B (zh) * 2015-12-07 2018-12-28 上海宇航系统工程研究所 一种可维修驱动锁定机构
CN107128480B (zh) * 2016-03-03 2022-05-10 北京臻迪机器人有限公司 一种飞行器脚架控制系统和方法
CN105866570A (zh) * 2016-03-25 2016-08-17 哈尔滨飞机工业集团有限责任公司 直升机起落架系统试验器
CN107521671B (zh) * 2016-06-22 2021-08-10 北京臻迪机器人有限公司 涡轮涡杆支架装置
US10549848B2 (en) * 2017-04-26 2020-02-04 Safran Landing Systems Canada Inc. Deployable and retractable shock strut
CN107314090A (zh) * 2017-07-04 2017-11-03 浙江捷昌线性驱动科技股份有限公司 一种可双向自锁的电动推杆
US11459094B2 (en) * 2017-09-29 2022-10-04 Georgia Tech Research Corporation Cable-driven four-bar link leg mechanism
FR3082825B1 (fr) * 2018-06-26 2020-09-04 Safran Landing Systems Mecanisme de verrouillage d’actionneur de roue
GB2578582A (en) * 2018-10-30 2020-05-20 Airbus Operations Ltd Landing gear
CN109774922B (zh) * 2019-01-22 2022-01-18 南京航空航天大学 一种变接地点的主起着陆装置
GB2581830A (en) * 2019-02-28 2020-09-02 Airbus Operations Ltd Landing gear system operation
GB2581825A (en) * 2019-02-28 2020-09-02 Airbus Operations Ltd Landing gear retraction
US11155345B2 (en) * 2019-11-11 2021-10-26 Goodrich Corporation Side folding and reforming linkage for landing gear
US12024277B2 (en) * 2020-02-06 2024-07-02 Goodrich Corporation Articulating truss configuration for aircraft landing gear
CN111284685B (zh) * 2020-03-12 2021-04-13 中航飞机起落架有限责任公司 一种空间收放起落架应急放下装置及应急放下方法
CN112441221B (zh) * 2020-12-04 2022-11-11 中航飞机起落架有限责任公司 一种双余度起落架备份放装置
EP4264086A1 (en) 2020-12-21 2023-10-25 CEF Industries, LLC Dual drive redundant load transmission device and process
US11787528B2 (en) 2020-12-23 2023-10-17 Whippany Actuation Systems Llc Jam free dual-redundant actuator lane changer system and process
USD1038174S1 (en) 2021-02-10 2024-08-06 Brunswick Corporation Cowling for an outboard motor
USD1042542S1 (en) 2021-06-02 2024-09-17 Brunswick Corporation Cowling for an outboard motor
USD983838S1 (en) 2021-06-14 2023-04-18 Brunswick Corporation Cowling for an outboard motor
US11713110B2 (en) * 2021-10-15 2023-08-01 Blended Wing Aircraft, Inc. Systems and methods for controlling landing gear of an aircraft
USD1023889S1 (en) 2022-01-14 2024-04-23 Brunswick Corporation Cowling on a deployable thruster for a marine vessel
US20230322370A1 (en) * 2022-04-06 2023-10-12 Goodrich Corporation Landing gear actuation system

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3904153A (en) * 1974-02-25 1975-09-09 Boeing Co Steerable and retractable aircraft nose landing gear assembly
JPS58502159A (ja) * 1981-12-18 1983-12-15 ラルス・インタ−ナショナル・ソシエテ・アノニム・ルクセンブルグ 2個のモ−タを備えた線形駆動装置
US4637272A (en) * 1985-10-28 1987-01-20 Sundstrand Corporation Ballscrew actuator
US5092539A (en) * 1989-10-13 1992-03-03 Bell Helicopter Textron Inc. Jam resistant ball screw actuator
US5128688A (en) * 1990-11-27 1992-07-07 Sperry Marine, Inc. Mast translation and rotation drive system utilizing a ball drive screw and nut assembly
US5144851A (en) * 1991-08-01 1992-09-08 Sundstrand Corp. Jam tolerant linear actuator
DE69933004D1 (de) * 1999-01-27 2006-10-12 Cooper Cameron Corp Elektrischer Stellantrieb
US6453761B1 (en) * 2000-11-16 2002-09-24 Thomson Saginaw Ball Screw Company, L.L.C. Direct attachment electric motor operated ball nut and screw linear actuator
FR2832685A1 (fr) * 2001-11-23 2003-05-30 Conception & Dev Michelin Sa Direction electrique pour vehicule, a redondance triple
FR2836669B1 (fr) * 2002-03-04 2004-12-03 Messier Bugatti Dispositif d'accrochage, notamment pour l'accrochage d'un train d'atterrissage d'aeronef ou d'une trappe de train d'atterrissage d'aeronef
US6791215B2 (en) * 2002-06-05 2004-09-14 Board Of Regents The University Of Texas System Fault tolerant linear actuator
US7098619B2 (en) * 2004-01-28 2006-08-29 Stridsberg Innovation Ab Actuator and movement linkage system
US7834494B2 (en) * 2004-06-04 2010-11-16 The Boeing Company Fault-tolerant electromechanical actuator having a torque sensing control system
US7190096B2 (en) * 2004-06-04 2007-03-13 The Boeing Company Fault-tolerant electro-mechanical actuator having motor armatures to drive a ram and having an armature release mechanism
FR2875475B1 (fr) * 2004-09-21 2008-02-08 Airbus France Sas Systeme de manoeuvre d'un train d'atterrissage pour aeronef et aeronef comportant un tel systeme
US20060266146A1 (en) * 2005-05-31 2006-11-30 Waide William M Direct drive electromechanical linear actuators
WO2007024220A1 (en) 2005-08-24 2007-03-01 Kollmorgen Corporation Failure-tolerant redundant actuator system
GB0604131D0 (en) 2006-03-01 2006-04-12 Airbus Uk Ltd Jam-tolerant actuator

Also Published As

Publication number Publication date
KR20110015036A (ko) 2011-02-14
WO2010009289A3 (en) 2010-05-20
US20100012779A1 (en) 2010-01-21
BRPI0915777B1 (pt) 2019-12-17
EP2318272B1 (en) 2012-03-07
CN102099248B (zh) 2014-07-02
WO2010009289A2 (en) 2010-01-21
CN102099248A (zh) 2011-06-15
CA2730926C (en) 2015-12-22
KR101279354B1 (ko) 2013-07-04
CA2730926A1 (en) 2010-01-21
EP2318272A2 (en) 2011-05-11
US8070094B2 (en) 2011-12-06
ATE548259T1 (de) 2012-03-15

Similar Documents

Publication Publication Date Title
BRPI0915777A2 (pt) sistema de trem de pouso, atuador de trem de pouso, e, método para ciclar um trem de pouso entre posições recolhida e estendida
ATE544675T1 (de) Landewerk für ein luftfahrzeug
US8827205B2 (en) Pneumatic blow-down actuator
KR101377174B1 (ko) 랜딩 기어, 항공기, 및 그 구현 방법
BRPI0419051A (pt) sistema de atuação de conversão de torre de tiltrotor compacto
EP1985536A3 (de) Steuerungseinrichtung eines Hubschrauber-Hauptrotors
JP4897803B2 (ja) 航空機の離陸引き起こしを支持する方法および装置
US20070007385A1 (en) Electric flight control surface actuation system electronic architecture
BRPI0810298A2 (pt) rebocador de avião sem barra de reboque
RU2014148320A (ru) Системы аварийного выпуска свободным падением под действием силы тяжести для узлов убирающегося шасси летательного аппарата
ATE481317T1 (de) Multimodale bemannte und unbemannte fahrzeugsysteme und -verfahren
BR112012005693A2 (pt) aparelho com capacidade propulsora com capacidade de mudança de tamanho ativa
WO2010118886A3 (de) Hochauftriebssystem eines flugzeugs, flugzeugsystem und propeller-flugzeug mit einem hochauftriebssystem
BR112017003126A2 (pt) freio de disco, pinça do freio e alavanca rotativa de freio
GB2495999B (en) Landing gear
FR2968375B1 (fr) Actionneur telescopique electromecanique.
US9004614B1 (en) Dual pressure control for a rotor brake actuator for vertical lift aircraft
BR112013026059A2 (pt) conjunto de válvula de controle de eixo mecânico de elevação para um veículo motorizado
DE602004001023D1 (de) System zur automatischen Steuerung von Hochauftriebsklappen eines Flugzeugs, insbesondere Flügelvorderkanten
JP2014190436A (ja) 車両用電動アクチュエータ
WO2011023980A3 (en) Main landing gear with rigid rear stay
CN105711818A (zh) 一种直升机脚蹬操纵机构
WO2007068413A3 (en) Method and device for providing automatic load alleviation to a high lift surface system, in particular to a landing flap system, of an aircraft
WO2011047998A3 (de) Steuervorrichtung für eine kabine eines luft- oder raumfahrzeuges, kabinenmanagementsystem und verfahren zum steuern einer kabine eines luft- oder raumfahrzeuges
CN107787290B (zh) 航空器起落装置

Legal Events

Date Code Title Description
B25A Requested transfer of rights approved

Owner name: CLAVERHAM LTD (GB)

B06T Formal requirements before examination [chapter 6.20 patent gazette]
B06A Patent application procedure suspended [chapter 6.1 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 17/12/2019, OBSERVADAS AS CONDICOES LEGAIS.