CN102343975B - 间接驱动的主动控制杆 - Google Patents

间接驱动的主动控制杆 Download PDF

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Publication number
CN102343975B
CN102343975B CN201110213011.4A CN201110213011A CN102343975B CN 102343975 B CN102343975 B CN 102343975B CN 201110213011 A CN201110213011 A CN 201110213011A CN 102343975 B CN102343975 B CN 102343975B
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CN
China
Prior art keywords
bar
passive
relative
feedback
positioner
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.)
Expired - Fee Related
Application number
CN201110213011.4A
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English (en)
Chinese (zh)
Other versions
CN102343975A (zh
Inventor
D·S·斯塔赫尼亚克
T·M·拉萨克
B·P·戴拉
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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
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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=CN102343975(B) "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 CN102343975A publication Critical patent/CN102343975A/zh
Application granted granted Critical
Publication of CN102343975B publication Critical patent/CN102343975B/zh
Expired - Fee Related 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

Landscapes

  • 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)
CN201110213011.4A 2010-07-28 2011-07-28 间接驱动的主动控制杆 Expired - Fee Related CN102343975B (zh)

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 (2)

Publication Number Publication Date
CN102343975A CN102343975A (zh) 2012-02-08
CN102343975B true CN102343975B (zh) 2016-02-03

Family

ID=44652353

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201110213011.4A Expired - Fee Related CN102343975B (zh) 2010-07-28 2011-07-28 间接驱动的主动控制杆

Country Status (7)

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

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* Cited by examiner, † Cited by third party
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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
GB2549272A (en) * 2016-04-11 2017-10-18 Bae Systems Plc Control systems
GB2549270B (en) 2016-04-11 2022-12-07 Bae Systems Plc Control systems and methods
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

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6659218B2 (en) * 2002-03-18 2003-12-09 Delphi Technologies, Inc. Steering system
CN101528539A (zh) * 2007-08-08 2009-09-09 莫戈公司 适用于电传飞行控制系统的控制杆和用于其中的连杆
US7648106B2 (en) * 2005-06-30 2010-01-19 Dassault Aviation Control system including two control columns that are coupled to enable controlled members to be placed in required positions

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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
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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
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
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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
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

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6659218B2 (en) * 2002-03-18 2003-12-09 Delphi Technologies, Inc. Steering system
US7648106B2 (en) * 2005-06-30 2010-01-19 Dassault Aviation Control system including two control columns that are coupled to enable controlled members to be placed in required positions
CN101528539A (zh) * 2007-08-08 2009-09-09 莫戈公司 适用于电传飞行控制系统的控制杆和用于其中的连杆

Also Published As

Publication number Publication date
JP2012030793A (ja) 2012-02-16
GB2482409B (en) 2013-07-10
GB201112856D0 (en) 2011-09-07
US9051045B2 (en) 2015-06-09
DE102011052206A1 (de) 2012-02-02
US20120025030A1 (en) 2012-02-02
GB2482409A (en) 2012-02-01
FR2963316A1 (fr) 2012-02-03
CN102343975A (zh) 2012-02-08
JP5882620B2 (ja) 2016-03-09
BRPI1103507A2 (pt) 2013-02-19

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PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
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GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
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Granted publication date: 20160203

Termination date: 20170728