IN2012DN03344A - - Google Patents

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Publication number
IN2012DN03344A
IN2012DN03344A IN3344DEN2012A IN2012DN03344A IN 2012DN03344 A IN2012DN03344 A IN 2012DN03344A IN 3344DEN2012 A IN3344DEN2012 A IN 3344DEN2012A IN 2012DN03344 A IN2012DN03344 A IN 2012DN03344A
Authority
IN
India
Application number
Other languages
English (en)
Inventor
Taylor Adam
Original Assignee
Bae Systems Plc
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=43447328&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=IN2012DN03344(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Priority claimed from GB0918200A external-priority patent/GB0918200D0/en
Priority claimed from EP09173421A external-priority patent/EP2311729A1/de
Application filed by Bae Systems Plc filed Critical Bae Systems Plc
Publication of IN2012DN03344A publication Critical patent/IN2012DN03344A/en

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
    • B64C13/10—Initiating means actuated personally comprising warning devices
    • 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
    • B64C13/40—Transmitting means with power amplification using fluid pressure
    • B64C13/46—Transmitting means with power amplification using fluid pressure with artificial feel

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Control Devices (AREA)
IN3344DEN2012 2009-10-19 2012-04-18 IN2012DN03344A (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB0918200A GB0918200D0 (en) 2009-10-19 2009-10-19 Tactile cueing apparatus
EP09173421A EP2311729A1 (de) 2009-10-19 2009-10-19 Taktile Signalisierungsvorrichtung
PCT/GB2010/051685 WO2011048399A1 (en) 2009-10-19 2010-10-08 Tactile cueing apparatus

Publications (1)

Publication Number Publication Date
IN2012DN03344A true IN2012DN03344A (de) 2015-10-23

Family

ID=43447328

Family Applications (1)

Application Number Title Priority Date Filing Date
IN3344DEN2012 IN2012DN03344A (de) 2009-10-19 2012-04-18

Country Status (6)

Country Link
US (1) US9381998B2 (de)
EP (1) EP2490936B2 (de)
AU (1) AU2010309603B2 (de)
CA (1) CA2778058C (de)
IN (1) IN2012DN03344A (de)
WO (1) WO2011048399A1 (de)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9102400B2 (en) * 2011-10-21 2015-08-11 Sikorsky Aircraft Corporation Methods and systems for providing constant-feel, multi-axis tactile cues
US9764830B2 (en) * 2012-02-10 2017-09-19 Bell Helicopter Textron Inc. Pilot control system with adjustable pedals
GB201220653D0 (en) * 2012-11-16 2013-01-02 Mcculloch Norman L Improvements in aircraft
US9969485B2 (en) * 2013-07-01 2018-05-15 Bae Systems Plc Inceptor and method for operating an inceptor
EP3069990B1 (de) * 2015-03-20 2017-01-11 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Vorrichtung zur erzeugung von künstlicher krafterfassung für ein fahrzeugsteuerungssystem eines fahrzeugs, insbesondere eines flugzeugs
US10618645B2 (en) * 2015-08-25 2020-04-14 Aerovironment, Inc. Ganged servo flight control system for an unmanned aerial vehicle
US10074245B2 (en) * 2017-01-10 2018-09-11 Woodward, Inc. Force feel using a brushless DC motor
US11117653B2 (en) * 2017-11-28 2021-09-14 Textron Innovations Inc. System and method for tactile cueing through rotorcraft pilot controls using variable friction and force gradient
US10967953B2 (en) * 2017-12-11 2021-04-06 The Boeing Company Combined active stick and control boost actuator system
US20200070966A1 (en) * 2018-09-05 2020-03-05 Bell Helicopter Textron Inc. Stuck in Detent Monitors for Collective and Cyclic Sticks
GB2577720B (en) * 2018-10-04 2023-04-19 Bae Systems Plc Oscilation system
EP3650354B1 (de) * 2018-11-12 2021-11-03 Ratier-Figeac SAS Schubregelungsanordnung
US11130567B2 (en) * 2019-02-25 2021-09-28 The Boeing Company Compactly mounted cyclic flight control for rotorcraft
FR3093320B1 (fr) * 2019-02-28 2021-01-29 Airbus Helicopters Mécanisme d’alerte haptique d’un pilote d’aéronef et aéronef.
EP3739230B1 (de) * 2019-05-16 2022-04-27 Ratier-Figeac SAS Aktuator mit auskuppelbarem ausgangshebel
US11148785B2 (en) 2019-08-22 2021-10-19 The Boeing Company Parallel actuation control system providing dual mode operator control inputs for a compound aircraft
FR3108313B1 (fr) * 2020-03-17 2023-05-26 Airbus Helicopters procédé de commande d’au moins une hélice d’un hélicoptère hybride et un hélicoptère hybride.
EP3882134B1 (de) 2020-03-20 2024-09-25 Ratier-Figeac SAS Cockpitsteuerorgansystem
US11623740B2 (en) 2021-02-19 2023-04-11 The Boeing Company Split-reference system and method for rapid re-trimming rate command of force trim release
RU2763198C1 (ru) * 2021-05-21 2021-12-28 Акционерное общество "Национальный центр вертолетостроения им. М.Л. Миля и Н.И. Камова" (АО "НЦВ Миль и Камов") Система управления вертолетом соосной схемы
EP4306431A1 (de) * 2022-07-15 2024-01-17 BAE SYSTEMS plc Elektronische einheit für ein taktiles hinweisgerät
KR20250037536A (ko) * 2022-07-15 2025-03-17 배 시스템즈 피엘시 촉각 큐잉 장치를 위한 전자 장치
US12371153B2 (en) 2022-07-18 2025-07-29 Textron Innovations Inc. Error monitors for collective and cyclic sticks
CN116424548B (zh) * 2023-03-30 2024-05-10 湖南山河华宇航空科技有限公司 一种电比例飞行操纵系统及控制方法和应用

Family Cites Families (18)

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Publication number Priority date Publication date Assignee Title
US2725203A (en) 1951-06-21 1955-11-29 Mcdonnell Aircraft Corp Aircraft control system with artificial feel
US2760739A (en) 1951-07-09 1956-08-28 James B Reichert Apparatus for controlling aircraft
GB742383A (en) 1951-10-10 1955-12-30 Boulton Aircraft Ltd Improvements in or relating to means for providing "feel" in power-operated flying control systems for aircraft
US2866611A (en) 1954-02-15 1958-12-30 Northrop Aircraft Inc Mechanical stick force producer
US2833496A (en) 1954-12-13 1958-05-06 Northrop Aircraft Inc Flight control system
GB1264330A (de) 1968-11-12 1972-02-23
US3945590A (en) 1975-01-23 1976-03-23 Sperry Rand Corporation Semi-automatic takeoff control system for aircraft
US4477044A (en) 1983-01-17 1984-10-16 The Boeing Company Elevator feel actuator
US5310138A (en) * 1991-12-30 1994-05-10 Alliedsignal Inc. Wing fold actuator system for aircraft
FR2718102B1 (fr) 1994-03-29 1996-06-28 Sfim Ind Procédé pour réaliser une loi d'effort antagoniste au mouvement d'un levier de commande de vol et son application au vérin de trim.
US5986359A (en) 1996-04-23 1999-11-16 Lear Automotive Dearborn, Inc. Power delivery circuit with short circuit protection
US5911390A (en) 1997-07-09 1999-06-15 Mcdonnell Douglas Corporation Bobweight assembly for establishing a force feedback on a manually movable control element
US6679458B2 (en) 2002-06-10 2004-01-20 The Boeing Company Split detent tactile cueing vehicle control system
US7108232B2 (en) * 2004-02-05 2006-09-19 Hoh Roger H Helicopter force-feel and stability augmentation system with parallel servo-actuator
US8002220B2 (en) * 2007-10-25 2011-08-23 Honeywell International Inc. Rate limited active pilot inceptor system and method
US8025256B2 (en) 2008-04-25 2011-09-27 The Boeing Company Precision adjust split detent for a vehicle
FR2946620A1 (fr) 2009-06-16 2010-12-17 Eurocopter France Procede d'aide au pilotage,moyen d'aide au pilotage et dispositif d'aide au pilotage d'un giravion utilisant ledit moyen d'aide au pilotage pour mettre en oeuvre ledit procede d'aide au pilotage.
FR2948629B1 (fr) 2009-07-28 2011-08-19 Eurocopter France Amortissement variable de restitution haptique pour chaine cinematique de changement d'attitude de vol d'un aeronef

Also Published As

Publication number Publication date
WO2011048399A1 (en) 2011-04-28
AU2010309603A1 (en) 2012-05-10
EP2490936A1 (de) 2012-08-29
EP2490936B2 (de) 2020-07-22
CA2778058A1 (en) 2011-04-28
CA2778058C (en) 2018-03-20
AU2010309603B2 (en) 2014-04-17
EP2490936B1 (de) 2015-06-10
US20120205494A1 (en) 2012-08-16
US9381998B2 (en) 2016-07-05

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