DE602007001165D1 - Aktiver Ruderpedalmechanismus mit Fremdobjektschlagtoleranz und Gelenkbremse - Google Patents

Aktiver Ruderpedalmechanismus mit Fremdobjektschlagtoleranz und Gelenkbremse

Info

Publication number
DE602007001165D1
DE602007001165D1 DE602007001165T DE602007001165T DE602007001165D1 DE 602007001165 D1 DE602007001165 D1 DE 602007001165D1 DE 602007001165 T DE602007001165 T DE 602007001165T DE 602007001165 T DE602007001165 T DE 602007001165T DE 602007001165 D1 DE602007001165 D1 DE 602007001165D1
Authority
DE
Germany
Prior art keywords
foreign object
pedal mechanism
object impact
rudder pedal
joint brake
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
DE602007001165T
Other languages
English (en)
Inventor
Donald J Christensen
Casey Hanlon
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Honeywell International Inc
Original Assignee
Honeywell International Inc
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 Honeywell International Inc filed Critical Honeywell International Inc
Publication of DE602007001165D1 publication Critical patent/DE602007001165D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02—Initiating means
    • B64C13/04—Initiating means actuated personally
    • B64C13/044—Initiating means actuated personally operated by feet, e.g. pedals
DE602007001165T 2006-06-30 2007-06-28 Aktiver Ruderpedalmechanismus mit Fremdobjektschlagtoleranz und Gelenkbremse Active DE602007001165D1 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US81818706P 2006-06-30 2006-06-30
US81818806P 2006-06-30 2006-06-30
US11/585,771 US7726611B2 (en) 2006-06-30 2006-10-23 Active rudder pedal mechanism with foreign object strike tolerance and articulating brake

Publications (1)

Publication Number Publication Date
DE602007001165D1 true DE602007001165D1 (de) 2009-07-09

Family

ID=38565523

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602007001165T Active DE602007001165D1 (de) 2006-06-30 2007-06-28 Aktiver Ruderpedalmechanismus mit Fremdobjektschlagtoleranz und Gelenkbremse

Country Status (4)

Country Link
US (1) US7726611B2 (de)
EP (1) EP1873057B1 (de)
BR (1) BRPI0705755A (de)
DE (1) DE602007001165D1 (de)

Families Citing this family (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009124032A1 (en) * 2008-03-31 2009-10-08 Honda Motor Co., Ltd. Pedal operated apparatus for controlling an aircraft nose wheel steering system
US8353484B2 (en) * 2009-11-10 2013-01-15 Textron Innovations, Inc. Cockpit rudder control mechanism for an aircraft
CN103057697B (zh) * 2013-01-07 2015-05-13 中国商用飞机有限责任公司 一种用于飞机的方向舵脚蹬控制装置和控制方法
US10180699B1 (en) 2013-08-08 2019-01-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration System, apparatus and method for pedal control
CN105711818B (zh) * 2014-12-03 2017-12-15 中国直升机设计研究所 一种直升机脚蹬操纵机构
CN105711817B (zh) * 2014-12-03 2017-11-21 中航通飞研究院有限公司 一种便携式手操纵飞机脚蹬装置
FR3029502B1 (fr) * 2014-12-08 2018-03-23 Airbus Operations Palonnier pour un aeronef
US10409315B2 (en) * 2016-03-04 2019-09-10 The Boeing Company Rudder control pedal assembly with linear pedal travel path
FR3049573B1 (fr) * 2016-04-05 2019-05-10 Airbus Operations Commande d'aeronef comprenant une pedale amelioree
CN109229345B (zh) * 2018-09-25 2021-11-02 陕西飞机工业（集团）有限公司 一种防误刹车的飞机脚操纵机构
CN110654531B (zh) * 2019-09-19 2022-05-03 中国商用飞机有限责任公司 一种用于飞机方向舵控制的脚蹬系统及其控制方法
US11396362B2 (en) 2019-11-01 2022-07-26 Woodward, Inc. Rudder and brake pedal assembly
CN112201114B (zh) * 2020-10-12 2021-11-19 浙江大学 一种基于齿轮齿条运动的大飞机脚蹬模拟装置
CN113460288B (zh) * 2021-09-03 2021-12-10 中国商用飞机有限责任公司 用于控制飞行器的主动式方向舵脚蹬组件以及飞行器
US11702193B1 (en) * 2022-04-28 2023-07-18 Beta Air, Llc Systems and methods for an electric vertical takeoff and landing aircraft braking system
US20240102540A1 (en) * 2022-09-28 2024-03-28 Safran Electronics & Defense, Avionics Usa, Llc Rudder and Brake Pedal Devices

Family Cites Families (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2424523A (en) * 1943-03-06 1947-07-22 Budd Co Aircraft operating mechanism
US2562974A (en) * 1945-11-30 1951-08-07 Sterry B Williams Rudder pedal adjustment
US2478546A (en) * 1946-10-11 1949-08-09 Cons Vultee Aircraft Corp Rudder pedal adjusting mechanism
US2585688A (en) * 1947-12-16 1952-02-12 Saulnier Raymond Aircraft rudder control column
US2697566A (en) * 1949-10-11 1954-12-21 Boeing Co Selective two or three control type system for aircraft
US2610006A (en) * 1950-11-18 1952-09-09 United Aircraft Corp Rudder pedal installation
US3377881A (en) * 1966-03-14 1968-04-16 United Aircraft Corp Foot control and adjustment linkage
US3919897A (en) * 1974-01-14 1975-11-18 Pacific Scientific Co Control line regulator surge lock assembly
US4198877A (en) * 1978-07-07 1980-04-22 The United States Of America As Represented By The Secretary Of The Air Force Control cable fail safe device
US4192476A (en) * 1978-07-14 1980-03-11 Northrop Corporation Rudder pedal adjustment system
US4484722A (en) * 1982-06-30 1984-11-27 The United States Of America As Represented By The Secretary Of The Air Force Translating rudder pedal system
US4470570A (en) * 1982-09-29 1984-09-11 The Boeing Company Control assembly for aircraft
GB8525631D0 (en) * 1985-10-17 1985-11-20 British Aerospace Aircraft flying control systems
US5056742A (en) * 1987-11-13 1991-10-15 The Boeing Company Modular rudder pedal and brake control assembly for aircraft
US4848708A (en) * 1987-11-13 1989-07-18 The Boeing Company Adjustable assembly for aircraft rudder, brake and nose landing gear steering control
US5797564A (en) * 1995-05-15 1998-08-25 The Boeing Company System for backdrive of flight deck controls during autopilot operation
KR0156339B1 (ko) * 1995-06-01 1999-02-18 배문한 경비행기의 브레이크 라더 페달 장치
JP3125677B2 (ja) * 1996-04-30 2001-01-22 トヨタ自動車株式会社 車両用ペダル支持構造
US5924331A (en) * 1997-07-08 1999-07-20 Mcdonnell Douglas Corporation Cable control system having stored energy fail-safe mechanism
US5996439A (en) * 1998-07-22 1999-12-07 General Motors Corporation Brake pedal mechanism
US6186025B1 (en) * 1999-03-24 2001-02-13 Teleflex, Inc. Break away pedal
FR2809373B1 (fr) * 2000-05-29 2002-08-09 Aerospatiale Matra Airbus Systeme de commande electrique pour une gouverne de direction d'aeronef
US6393934B1 (en) * 2000-06-21 2002-05-28 Teleflex Incorporated Break-away pedal with ball swivel snap-in
US7059563B2 (en) * 2003-06-03 2006-06-13 The Boeing Company Systems, apparatuses, and methods for moving aircraft control surfaces
US6981409B2 (en) * 2003-08-01 2006-01-03 The Boeing Company Control surface controller force measurement system
US6923405B2 (en) * 2003-11-17 2005-08-02 The Boeing Company Enhanced rudder control system
US7644893B2 (en) * 2006-02-15 2010-01-12 Sikorsky Aircraft Corporation Full authority fly-by-wire pedal system

Also Published As

Publication number Publication date
US20080023591A1 (en) 2008-01-31
EP1873057A1 (de) 2008-01-02
EP1873057B1 (de) 2009-05-27
BRPI0705755A (pt) 2008-06-03
US7726611B2 (en) 2010-06-01

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Legal Events

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8364 No opposition during term of opposition