MX336233B - Dispositivo de operación de superficie de control para aeronave. - Google Patents

Dispositivo de operación de superficie de control para aeronave.

Info

Publication number
MX336233B
MX336233B MX2013004326A MX2013004326A MX336233B MX 336233 B MX336233 B MX 336233B MX 2013004326 A MX2013004326 A MX 2013004326A MX 2013004326 A MX2013004326 A MX 2013004326A MX 336233 B MX336233 B MX 336233B
Authority
MX
Mexico
Prior art keywords
control surface
drive
mounting assembly
operating device
aircraft
Prior art date
Application number
MX2013004326A
Other languages
English (en)
Other versions
MX2013004326A (es
Inventor
Minoru Uchida
Hiroshi Yamanouchi
Original Assignee
Honda Patents & Tech North Am
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 Honda Patents & Tech North Am filed Critical Honda Patents & Tech North Am
Publication of MX2013004326A publication Critical patent/MX2013004326A/es
Publication of MX336233B publication Critical patent/MX336233B/es

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/02—Mounting or supporting thereof
    • 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
    • Y02T50/30—Wing lift efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
  • Mechanical Control Devices (AREA)

Abstract

Una dispositivo de operación de superficie de control para aeronave se proporcionó para una superficie de control de una porción de armazón de aeronave para moverse entre una posición retraída y una posición extendida. El dispositivo de operación de superficie de control para aeronave incluye una unidad de instalación de superficie de control que asegura de forma móvil la superficie de control a la posición de armazón de aeronave, un brazo impulsor giratorio sobre un eje impulsor en relación con la porción de armazón de aeronave, un propulsor para girar el impulsor, y un mecanismo impulsor que conecta al brazo impulsor con la unidad de instalación de superficie de control. El mecanismo impulsor tiene un extremo de control conectado a la unidad de instalación de superficie de control y un extremo de impulsión conectado al brazo impulsor mediante una junta de soporte impulsor. El mecanismo impulsor conecta al brazo impulsor y la unidad de instalación de superficie de control de forma que la rotación del brazo impulsor causa el movimiento de extensión o retracción de la superficie de control.
MX2013004326A 2010-10-18 2011-10-18 Dispositivo de operación de superficie de control para aeronave. MX336233B (es)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US39426310P 2010-10-18 2010-10-18
US13/275,676 US8596582B2 (en) 2010-10-18 2011-10-18 Aircraft control surface operating device
PCT/US2011/056692 WO2012054470A1 (en) 2010-10-18 2011-10-18 Aircraft control surface operating device

Publications (2)

Publication Number Publication Date
MX2013004326A MX2013004326A (es) 2013-08-29
MX336233B true MX336233B (es) 2016-01-12

Family

ID=45933295

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2013004326A MX336233B (es) 2010-10-18 2011-10-18 Dispositivo de operación de superficie de control para aeronave.

Country Status (6)

Country Link
US (1) US8596582B2 (es)
EP (1) EP2630033B1 (es)
CA (1) CA2814133C (es)
ES (1) ES2541862T3 (es)
MX (1) MX336233B (es)
WO (1) WO2012054470A1 (es)

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US8998132B2 (en) * 2011-11-30 2015-04-07 Lockheed Martin Corporation Aerodynamic wing load distribution control
GB201120992D0 (en) * 2011-12-07 2012-01-18 Airbus Uk Ltd Aircraft rib assembly
EP2844886B1 (en) * 2012-04-30 2018-11-07 Roller Bearing Company of America, Inc. Hybrid bearing assembly with rolling elements and plain bearing
US9163648B2 (en) 2013-02-27 2015-10-20 Woodward, Inc. Rotary piston type actuator with a central actuation assembly
US9593696B2 (en) 2013-02-27 2017-03-14 Woodward, Inc. Rotary piston type actuator with hydraulic supply
US9234535B2 (en) 2013-02-27 2016-01-12 Woodward, Inc. Rotary piston type actuator
US9476434B2 (en) 2013-02-27 2016-10-25 Woodward, Inc. Rotary piston type actuator with modular housing
US9816537B2 (en) 2013-02-27 2017-11-14 Woodward, Inc. Rotary piston type actuator with a central actuation assembly
US8955425B2 (en) 2013-02-27 2015-02-17 Woodward, Inc. Rotary piston type actuator with pin retention features
US9631645B2 (en) 2013-02-27 2017-04-25 Woodward, Inc. Rotary piston actuator anti-rotation configurations
EP2883787B1 (de) * 2013-12-12 2019-06-12 Airbus Defence and Space GmbH Antriebsmechanismus für eine verformbare Tragflächenvorderkante
US20150360768A1 (en) * 2014-06-12 2015-12-17 Troy A. Woodland Mounting assembly for fully automatic slat
CN109070994A (zh) * 2016-04-04 2018-12-21 航空伙伴股份有限公司 用于自适应翼型件的致动器
AT518606A1 (de) * 2016-04-29 2017-11-15 Facc Ag Aerodynamischer Profilkörper für ein Flugzeug
EP3241740B1 (en) * 2016-05-03 2020-08-19 Airbus Operations GmbH System for driving a slat device of an aircraft wing
US11046425B2 (en) * 2016-05-20 2021-06-29 Bombardier Inc. Apparatus and methods for actuating a double-slotted flap using a slave screw
US10710702B2 (en) 2016-08-12 2020-07-14 Aviation Partners, Inc. Shape adaptive airfoil
BR102016020505B1 (pt) * 2016-09-05 2022-08-02 Embraer S.A Mecanismo de deflexão de painéis de flaps de aeronave
WO2018102183A1 (en) * 2016-12-03 2018-06-07 Ge Aviation Systems Llc Spherical bearing system
US10611462B2 (en) * 2017-08-18 2020-04-07 The Boeing Company Actuator assemblies for control surfaces of an aircraft, aircraft including the actuator assemblies, and methods of utilizing the same
US10974816B2 (en) * 2017-09-28 2021-04-13 The Boeing Company High-fowler flap actuation apparatus and related methods
CN108163183B (zh) * 2017-10-23 2020-11-10 中国商用飞机有限责任公司北京民用飞机技术研究中心 一种基于副翼连接接头位置变化的操纵效率提高的方法
GB201815106D0 (en) * 2018-09-17 2018-10-31 Airbus Operations Ltd Improved aircraft wing and flight control surface
CN110294102B (zh) * 2019-04-26 2023-05-23 庆安集团有限公司 一体式襟副翼的复合运动机构
US11199248B2 (en) 2019-04-30 2021-12-14 Woodward, Inc. Compact linear to rotary actuator
EP3757410B1 (en) * 2019-06-28 2021-11-03 Airbus Operations (S.A.S.) Bearing assembly of a hinge coupling a first component and a second component
US11260960B2 (en) * 2019-07-09 2022-03-01 The Boeing Company Flap actuation system for aircraft
EP4133186B1 (en) 2020-04-08 2025-10-01 Woodward, Inc. Rotary piston type actuator with a central actuation assembly
CN112572768A (zh) * 2020-12-18 2021-03-30 中国电子科技集团公司第三十八研究所 一种无人机全动垂尾的操纵机构
US20220266998A1 (en) * 2021-02-19 2022-08-25 Lilium Eaircraft Gmbh Aircraft
US11932377B2 (en) * 2021-06-04 2024-03-19 The Boeing Company Actuation mechanism for controlling aircraft surfaces

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US4542869A (en) * 1983-06-23 1985-09-24 Mcdonnell Douglas Corporation Flap mechanism
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US5836550A (en) * 1996-11-27 1998-11-17 Boeing Company Mechanism for streamwise fowler deployment of the wing trailing or leading edge
US6464176B2 (en) * 2000-07-26 2002-10-15 Honda Giken Kogyo Kabushiki Kaisha Flap operating device
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US20060071441A1 (en) * 2004-10-06 2006-04-06 William Mathis Lower control arm kit for vehicle with four link rear suspension
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US20110236877A1 (en) * 2010-03-26 2011-09-29 Da-Jeng Yao Biosensor and method using the same to perform a biotest

Also Published As

Publication number Publication date
CA2814133C (en) 2017-02-28
AU2011317260A8 (en) 2015-12-03
EP2630033B1 (en) 2015-07-01
CA2814133A1 (en) 2012-04-26
ES2541862T3 (es) 2015-07-27
US8596582B2 (en) 2013-12-03
MX2013004326A (es) 2013-08-29
WO2012054470A1 (en) 2012-04-26
US20120091283A1 (en) 2012-04-19
AU2011317260A1 (en) 2013-05-02
EP2630033A1 (en) 2013-08-28
EP2630033A4 (en) 2014-07-02
AU2011317260B2 (en) 2015-08-13

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