DE102011052206A1 - Inaktive Direktantriebs-Steuersäule - Google Patents

Inaktive Direktantriebs-Steuersäule Download PDF

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Publication number
DE102011052206A1
DE102011052206A1 DE102011052206A DE102011052206A DE102011052206A1 DE 102011052206 A1 DE102011052206 A1 DE 102011052206A1 DE 102011052206 A DE102011052206 A DE 102011052206A DE 102011052206 A DE102011052206 A DE 102011052206A DE 102011052206 A1 DE102011052206 A1 DE 102011052206A1
Authority
DE
Germany
Prior art keywords
feedback
stick
assembly
relative
passive
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.)
Withdrawn
Application number
DE102011052206A
Other languages
German (de)
English (en)
Inventor
Darryl S. Stachniak
Thomas M. Rusak
Brian P. Dyra
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.)
Woodward MPC Inc
Original Assignee
Woodward MPC 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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=44652353&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE102011052206(A1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Woodward MPC Inc filed Critical Woodward MPC Inc
Publication of DE102011052206A1 publication Critical patent/DE102011052206A1/de
Withdrawn legal-status Critical Current

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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
    • B64C13/12—Dual control apparatus
    • 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
    • B64C13/042—Initiating means actuated personally operated by hand
    • B64C13/0421—Initiating means actuated personally operated by hand control sticks for primary flight controls
    • 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
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B64C13/503—Fly-by-Wire
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05G—CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
    • G05G11/00—Manually-actuated control mechanisms provided with two or more controlling members co-operating with one single controlled member
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05G—CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
    • G05G5/00—Means for preventing, limiting or returning the movements of parts of a control mechanism, e.g. locking controlling member
    • G05G5/03—Means for enhancing the operator's awareness of arrival of the controlling member at a command or datum position; Providing feel, e.g. means for creating a counterforce
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05G—CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY
    • G05G7/00—Manually-actuated control mechanisms provided with one single controlling member co-operating with one single controlled member; Details thereof

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  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Control Devices (AREA)
  • Transmission Devices (AREA)
DE102011052206A 2010-07-28 2011-07-27 Inaktive Direktantriebs-Steuersäule Withdrawn DE102011052206A1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/845,160 2010-07-28
US12/845,160 US9051045B2 (en) 2010-07-28 2010-07-28 Indirect drive active control column

Publications (1)

Publication Number Publication Date
DE102011052206A1 true DE102011052206A1 (de) 2012-02-02

Family

ID=44652353

Family Applications (1)

Application Number Title Priority Date Filing Date
DE102011052206A Withdrawn DE102011052206A1 (de) 2010-07-28 2011-07-27 Inaktive Direktantriebs-Steuersäule

Country Status (7)

Country Link
US (1) US9051045B2 (enExample)
JP (1) JP5882620B2 (enExample)
CN (1) CN102343975B (enExample)
BR (1) BRPI1103507A2 (enExample)
DE (1) DE102011052206A1 (enExample)
FR (1) FR2963316A1 (enExample)
GB (1) GB2482409B (enExample)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9126676B2 (en) 2011-10-28 2015-09-08 Woodward Mpc, Inc. Compact two axis gimbal for control stick
FR2993065B1 (fr) * 2012-07-09 2014-08-29 Ratier Figeac Soc Dispositif de conjugaison d'effort entre organes de pilotage, organe de pilotage et aeronef
US10532693B2 (en) * 2013-08-30 2020-01-14 Itc Incorporated Diffused flexible LED linear light assembly
DE102014103988A1 (de) * 2014-03-24 2015-09-24 Elobau Gmbh & Co. Kg Joystick mit intrinsisch sicherem Force-Feedback
US10006615B2 (en) * 2014-05-30 2018-06-26 Oelo, LLC Lighting system and method of use
US9446838B2 (en) * 2014-08-14 2016-09-20 Gulfstream Aerospace Corporation Systems for inceptor control in fly-by-wire aircraft systems
GB2549270B (en) 2016-04-11 2022-12-07 Bae Systems Plc Control systems and methods
GB2549272A (en) * 2016-04-11 2017-10-18 Bae Systems Plc Control systems
CN107097934B (zh) * 2017-03-30 2019-04-05 南京航空航天大学 一种飞机侧杆系统主被动模式的切换方法
DE102017115863A1 (de) * 2017-07-14 2019-01-17 Fernsteuergeräte Kurt Oelsch GmbH Bedienhebel mit Kulissenführung
CN107719643B (zh) * 2017-09-29 2020-06-16 兰州飞行控制有限责任公司 一种电传飞机侧杆操纵机构
WO2019122807A1 (en) * 2017-12-21 2019-06-27 Bae Systems Plc Aircraft control systems
FR3093320B1 (fr) * 2019-02-28 2021-01-29 Airbus Helicopters Mécanisme d’alerte haptique d’un pilote d’aéronef et aéronef.
US11396362B2 (en) 2019-11-01 2022-07-26 Woodward, Inc. Rudder and brake pedal assembly
CN114162309B (zh) * 2021-11-30 2024-06-04 中国商用飞机有限责任公司 主动侧杆系统

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GB126568A (en) 1918-10-08 1919-05-15 James Frederick Verner Improvements in Aeroplane Controls.
US2955356A (en) * 1944-06-08 1960-10-11 Sperry Rand Corp Bombsight
GB827089A (en) 1955-03-03 1960-02-03 Honeywell Regulator Co Improvements in control systems for dirigible craft
GB925471A (en) 1959-08-31 1963-05-08 William Warren Triggs C B E Manual and automatic hydraulic servomechanism
US3415469A (en) * 1966-09-22 1968-12-10 George G. Spratt Airplane
US3902379A (en) 1973-12-03 1975-09-02 Us Navy High load, quick-disconnect link
US4228386A (en) * 1978-06-02 1980-10-14 Sperry Corporation Aircraft servoactuator apparatus
FR2525000A1 (fr) 1982-04-07 1983-10-14 Aerospatiale Manche de commande debrayable pour copilote d'aeronef
FR2558136B1 (fr) 1984-01-12 1986-04-25 Aerospatiale Dispositif de commande pourvu de deux manches conjugues et actionnes respectivement par une main gauche et par une main droite
US4716399A (en) 1985-01-14 1987-12-29 The Boeing Company Optomechanical control apparatus
FR2583017B1 (fr) 1985-06-07 1987-09-18 Aerospatiale Dispositif de commande pourvu de deux manches couples
US4717098A (en) * 1986-05-19 1988-01-05 Mcdonnell Douglas Corporation Actuator for a g-limiter override
US5149023A (en) 1991-07-12 1992-09-22 The Boeing Company Mechanically-linked side stick controllers with isolated pitch and roll control movement
US5456428A (en) 1993-07-21 1995-10-10 Honeywell Inc. Mechanically linked active sidesticks
US5489830A (en) * 1994-09-09 1996-02-06 Mcdonnell Douglas Corporation Control system with loadfeel and backdrive
FR2728537A1 (fr) * 1994-12-21 1996-06-28 Eurocopter France Dispositif pour l'actionnement d'un organe commande pour un aeronef, tel que notamment un helicoptere, a commandes de vol electriques
US7027032B2 (en) * 1995-12-01 2006-04-11 Immersion Corporation Designing force sensations for force feedback computer applications
US6219032B1 (en) * 1995-12-01 2001-04-17 Immersion Corporation Method for providing force feedback to a user of an interface device based on interactions of a controlled cursor with graphical elements in a graphical user interface
FR2756392B1 (fr) 1996-11-22 1999-01-22 Aerospatiale Systeme de couplage de manches de commande
JP3065603B1 (ja) * 1999-03-18 2000-07-17 株式会社コミュータヘリコプタ先進技術研究所 操縦装置
US6572055B1 (en) 1999-08-10 2003-06-03 Bombardier Aerospace Corporation Hydrostatic sidestick coupling
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US6459228B1 (en) 2001-03-22 2002-10-01 Mpc Products Corporation Dual input servo coupled control sticks
US6659218B2 (en) * 2002-03-18 2003-12-09 Delphi Technologies, Inc. Steering system
FR2888009B1 (fr) * 2005-06-30 2007-09-07 Dassault Aviat Dispositif de commande comportant deux manches couples pour permettre de placer des organes commandes dans des positions souhaitees
DE602005016471D1 (de) 2005-11-30 2009-10-15 Svend Egenfeldt Fernsteuersystem
US7559510B1 (en) * 2006-09-27 2009-07-14 Rockwell Collins, Inc. Elevator variable feel unit
US7658349B2 (en) 2006-10-26 2010-02-09 Honeywell International Inc. Pilot flight control stick haptic feedback system and method
US7759894B2 (en) * 2006-10-26 2010-07-20 Honeywell International Inc. Cogless motor driven active user interface haptic feedback system
JP4772712B2 (ja) 2007-02-19 2011-09-14 本田技研工業株式会社 車両のペダル式操作装置
KR101420353B1 (ko) * 2007-08-08 2014-07-16 무그 인코포레이티드 플라이-바이-와이어 비행 조종 시스템 내에서 사용되도록 구성된 조종간 및 이에 사용되는 링크 장치
US8078340B2 (en) 2007-11-12 2011-12-13 Honeywell International Inc. Active user interface haptic feedback and linking control system using either force or position data
US9156546B2 (en) 2008-03-11 2015-10-13 The Boeing Company Active-inceptor tactile-cueing hands-off rate-limit
GB2465761A (en) 2008-11-27 2010-06-02 Gm Global Tech Operations Inc A clutch pedal with a spring having an adjustable spring characteristic
US8814103B2 (en) 2010-07-28 2014-08-26 Woodward Mpc, Inc. Position control system for cross coupled operation of fly-by-wire control columns

Also Published As

Publication number Publication date
FR2963316A1 (fr) 2012-02-03
US20120025030A1 (en) 2012-02-02
JP2012030793A (ja) 2012-02-16
GB2482409B (en) 2013-07-10
CN102343975B (zh) 2016-02-03
CN102343975A (zh) 2012-02-08
US9051045B2 (en) 2015-06-09
GB2482409A (en) 2012-02-01
BRPI1103507A2 (pt) 2013-02-19
JP5882620B2 (ja) 2016-03-09
GB201112856D0 (en) 2011-09-07

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R082 Change of representative

Representative=s name: FISH & RICHARDSON P.C., DE

R012 Request for examination validly filed
R002 Refusal decision in examination/registration proceedings
R119 Application deemed withdrawn, or ip right lapsed, due to non-payment of renewal fee