DE60111693D1 - Hydraulische Steuerung für eine Trimmungsklappe - Google Patents

Hydraulische Steuerung für eine Trimmungsklappe

Info

Publication number
DE60111693D1
DE60111693D1 DE60111693T DE60111693T DE60111693D1 DE 60111693 D1 DE60111693 D1 DE 60111693D1 DE 60111693 T DE60111693 T DE 60111693T DE 60111693 T DE60111693 T DE 60111693T DE 60111693 D1 DE60111693 D1 DE 60111693D1
Authority
DE
Germany
Prior art keywords
hydraulic control
trim flap
trim
flap
hydraulic
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
DE60111693T
Other languages
English (en)
Other versions
DE60111693T2 (de
Inventor
Kenneth Edward Hart
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 HRT Inc
Original Assignee
Woodward HRT 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 Woodward HRT Inc filed Critical Woodward HRT Inc
Application granted granted Critical
Publication of DE60111693D1 publication Critical patent/DE60111693D1/de
Publication of DE60111693T2 publication Critical patent/DE60111693T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • B64C13/24—Transmitting means
    • B64C13/38—Transmitting means with power amplification
    • B64C13/50—Transmitting means with power amplification using electrical energy
    • B64C13/505—Transmitting means with power amplification using electrical energy having duplication or stand-by provisions

Landscapes

  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Servomotors (AREA)
  • Flow Control (AREA)
DE60111693T 2000-08-24 2001-03-29 Hydraulische Steuerung für eine Trimmungsklappe Expired - Fee Related DE60111693T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/645,188 US6439512B1 (en) 2000-08-24 2000-08-24 All-hydraulic powered horizontal stabilizer trim control surface position control system
US645188 2000-08-24

Publications (2)

Publication Number Publication Date
DE60111693D1 true DE60111693D1 (de) 2005-08-04
DE60111693T2 DE60111693T2 (de) 2006-05-04

Family

ID=24587980

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60111693T Expired - Fee Related DE60111693T2 (de) 2000-08-24 2001-03-29 Hydraulische Steuerung für eine Trimmungsklappe

Country Status (4)

Country Link
US (1) US6439512B1 (de)
EP (1) EP1182134B1 (de)
JP (1) JP4116271B2 (de)
DE (1) DE60111693T2 (de)

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US6578425B2 (en) * 2001-05-29 2003-06-17 Honeywell Inc. Apparatus and method for verifying the dynamic stiffness capability of hydraulic servo actuators
US6799739B1 (en) * 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
KR100840613B1 (ko) * 2003-11-25 2008-06-23 국방과학연구소 항공기 자동러더트림제어 장치의 테스트 장치
US7098619B2 (en) * 2004-01-28 2006-08-29 Stridsberg Innovation Ab Actuator and movement linkage system
US7494094B2 (en) 2004-09-08 2009-02-24 The Boeing Company Aircraft wing systems for providing differential motion to deployable lift devices
US7264206B2 (en) 2004-09-30 2007-09-04 The Boeing Company Leading edge flap apparatuses and associated methods
US7338018B2 (en) 2005-02-04 2008-03-04 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
US7721999B2 (en) 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems and associated methods
JP2007056998A (ja) * 2005-08-24 2007-03-08 Shin Caterpillar Mitsubishi Ltd 旋回駆動装置および作業機械
US7708231B2 (en) 2005-11-21 2010-05-04 The Boeing Company Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
US7475854B2 (en) 2005-11-21 2009-01-13 The Boeing Company Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods
US20080237402A1 (en) * 2005-12-19 2008-10-02 Marc Ausman Aircraft trim safety system and backup controls
US8210206B2 (en) * 2007-11-27 2012-07-03 Woodward Hrt, Inc. Dual redundant servovalve
US7954769B2 (en) 2007-12-10 2011-06-07 The Boeing Company Deployable aerodynamic devices with reduced actuator loads, and related systems and methods
US7766282B2 (en) 2007-12-11 2010-08-03 The Boeing Company Trailing edge device catchers and associated systems and methods
US8070091B2 (en) * 2008-10-08 2011-12-06 Honeywell International Inc. Electromechanical actuation system and method
US8382045B2 (en) 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
RU2500576C2 (ru) * 2011-06-08 2013-12-10 Открытое акционерное общество "Павловский машиностроительный завод ВОСХОД" (ОАО "ПМЗ ВОСХОД") Электрогидравлический рулевой привод
FR2978423B1 (fr) * 2011-07-28 2014-12-19 Airbus Operations Sas Procede et dispositif de detection de l'embarquement d'une gouverne d'aeronef
RU2474732C1 (ru) * 2011-10-10 2013-02-10 Открытое акционерное общество "Конструкторское Бюро Промышленной Автоматики" Дроссельный электрогидропривод
US9803663B2 (en) 2011-10-27 2017-10-31 Parker-Hannifin Corporation Telescoping fluid porting tube
CN102637039B (zh) * 2012-04-19 2013-09-18 中国船舶重工集团公司第七一〇研究所 海洋拖曳线阵三翼定位方法
RU2483229C1 (ru) * 2012-04-23 2013-05-27 Открытое акционерное общество "Конструкторское Бюро Промышленной Автоматики" Дроссельный электрогидропривод
US9611031B2 (en) * 2013-08-30 2017-04-04 Rosemount Aerospace Inc. Flutter control actuator
US10450056B2 (en) * 2016-07-19 2019-10-22 The Boeing Company Horizontal stabilizer trim actuator systems and methods
US10543903B2 (en) * 2016-08-31 2020-01-28 The Boeing Company Actuators for high lift devices on aircraft
EP3505440B1 (de) 2017-12-28 2022-03-09 Goodrich Actuation Systems SAS Höhenleitwerkverkleidungs-stellgliedbaugruppe
CN108109465A (zh) * 2017-12-29 2018-06-01 天津华翼蓝天科技股份有限公司 一种飞行模拟器的仿真方向舵配平旋钮装置
EP3650336A1 (de) * 2018-11-12 2020-05-13 Goodrich Actuation Systems SAS Trimsteuerungssystem
EP4305653A1 (de) 2021-03-12 2024-01-17 Essex Industries, Inc. Wippschalter
US11688568B2 (en) 2021-03-15 2023-06-27 Essex Industries, Inc. Five-position switch

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US4133250A (en) 1977-06-22 1979-01-09 Pneumo Corporation Combined feedback control system
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US4231284A (en) 1978-08-31 1980-11-04 Textron, Inc. Load equilization feedback for parallel channel servo actuators
US4807517A (en) 1982-09-30 1989-02-28 Allied-Signal Inc. Electro-hydraulic proportional actuator
EP0152714B1 (de) * 1984-01-09 1987-04-01 AEROSPATIALE Société Nationale Industrielle Flugsteuereinrichtung für Luftfahrzeuge
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JPS63291772A (ja) 1987-05-26 1988-11-29 Komatsu Ltd 油圧式ステアリング装置
US5074495A (en) 1987-12-29 1991-12-24 The Boeing Company Load-adaptive hybrid actuator system and method for actuating control surfaces
JP3382981B2 (ja) * 1992-11-12 2003-03-04 帝人製機株式会社 舵面の制御装置
US5848612A (en) 1997-11-25 1998-12-15 Sargent Controls & Aerospace/Dover Diversified Inc. Servovalve employing a rotatable feedback linkage

Also Published As

Publication number Publication date
JP4116271B2 (ja) 2008-07-09
JP2002114196A (ja) 2002-04-16
EP1182134B1 (de) 2005-06-29
DE60111693T2 (de) 2006-05-04
EP1182134A2 (de) 2002-02-27
EP1182134A3 (de) 2003-01-15
US6439512B1 (en) 2002-08-27

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee