ATE329825T1 - Betätigungssystem für ein aerodynamisches ruder - Google Patents

Betätigungssystem für ein aerodynamisches ruder

Info

Publication number
ATE329825T1
ATE329825T1 AT02258426T AT02258426T ATE329825T1 AT E329825 T1 ATE329825 T1 AT E329825T1 AT 02258426 T AT02258426 T AT 02258426T AT 02258426 T AT02258426 T AT 02258426T AT E329825 T1 ATE329825 T1 AT E329825T1
Authority
AT
Austria
Prior art keywords
airstream
load
control surface
horn member
positions
Prior art date
Application number
AT02258426T
Other languages
English (en)
Inventor
Kendall G Young
Stephen L Pauletti
Original Assignee
Northrop Grumman Corp
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 Northrop Grumman Corp filed Critical Northrop Grumman Corp
Application granted granted Critical
Publication of ATE329825T1 publication Critical patent/ATE329825T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • 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
    • B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
    • B64C13/28—Transmitting means without power amplification or where power amplification is irrelevant mechanical
    • B64C13/34—Transmitting means without power amplification or where power amplification is irrelevant mechanical using toothed gearing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Toys (AREA)
  • Vehicle Body Suspensions (AREA)
  • Transmission Devices (AREA)
AT02258426T 2001-11-28 2002-11-22 Betätigungssystem für ein aerodynamisches ruder ATE329825T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/996,182 US6467733B1 (en) 2001-11-28 2001-11-28 Aerodynamic control surface system

Publications (1)

Publication Number Publication Date
ATE329825T1 true ATE329825T1 (de) 2006-07-15

Family

ID=25542595

Family Applications (1)

Application Number Title Priority Date Filing Date
AT02258426T ATE329825T1 (de) 2001-11-28 2002-11-22 Betätigungssystem für ein aerodynamisches ruder

Country Status (6)

Country Link
US (1) US6467733B1 (de)
EP (1) EP1316501B1 (de)
AT (1) ATE329825T1 (de)
DE (1) DE60212303T2 (de)
IL (1) IL153055A (de)
RU (1) RU2296694C2 (de)

Families Citing this family (32)

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DE102005038856A1 (de) 2005-08-17 2007-02-22 Airbus Deutschland Gmbh Kontinuierlicher Rumpfanschluss
DE102008047793B4 (de) * 2008-09-17 2017-03-30 Airbus Defence and Space GmbH Lasteinleitungselement
US9127908B2 (en) 2009-02-02 2015-09-08 Aero Vironment, Inc. Multimode unmanned aerial vehicle
AU2010325108B2 (en) * 2009-09-09 2016-09-01 Aerovironment, Inc. Elevon control system
KR20120113210A (ko) 2009-09-09 2012-10-12 에어로바이론먼트, 인크. 휴대용 ｒｆ 투명 발사관을 구비한 원격 조종 무인 항공기 포성 억제 발사장치를 위한 시스템 및 장치
WO2011054047A1 (en) * 2009-11-04 2011-05-12 John Mcmurray Clark A compound motion structure
DE102009051983A1 (de) 2009-11-05 2011-05-12 Airbus Operations Gmbh Tragflügel eines Flugzeugs
US8695925B2 (en) * 2010-12-15 2014-04-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Elastically deformable side-edge link for trailing-edge flap aeroacoustic noise reduction
US9227721B1 (en) * 2011-10-07 2016-01-05 The United States of America as represented by the Administrator of the National Aeronautics & Space Administration (NASA) Variable camber continuous aerodynamic control surfaces and methods for active wing shaping control
IL216345A (en) * 2011-11-14 2017-09-28 Israel Aerospace Ind Ltd Wing and the devices for it
US8590834B1 (en) * 2011-11-14 2013-11-26 The Boeing Company Aircraft control surface actuation system with helical actuation path
CN102582825B (zh) * 2012-02-14 2013-12-25 西北工业大学 一种用于飞机机翼表面的密封机构
US8814100B2 (en) * 2012-04-19 2014-08-26 The Boeing Company Continuous moldline technology (CMT) elastomeric control surface
FR2992629B1 (fr) * 2012-06-27 2014-09-12 Airbus Operations Sas Dispositif de liaison mecanique d'une gouverne a un element structural fixe d'aeronef et element de voilure d'aeronef equipe de ce dispositif
UA79830U (ru) * 2013-03-12 2013-04-25 Юрий Григорьевич Сидоренко Привод управления подвижной аэродинамической поверхностью крыла самолета
US10017243B2 (en) * 2013-09-24 2018-07-10 The Boeing Company Adaptive trailing edge actuator system and method
US9038943B1 (en) * 2014-04-11 2015-05-26 Ralph F. Morris Safety aileron system
FR3022215B1 (fr) * 2014-06-13 2016-05-27 Sagem Defense Securite Actionneur pour surface de vol et ensemble de guidage d'un aeronef comprenant un tel actionneur
CN105292443A (zh) * 2015-11-27 2016-02-03 深圳飞马机器人科技有限公司 一种机翼副翼驱动结构
US9975623B2 (en) * 2016-03-08 2018-05-22 Northrop Grumman Systems Corporation Elastomeric transition
US11745857B2 (en) 2016-03-30 2023-09-05 Goodrich Actuation Systems Sas Aircraft force-fight mechanism
EP3225540B1 (de) * 2016-03-30 2020-11-18 Goodrich Actuation Systems SAS Kraftkampfabschwächung
JP2020500761A (ja) * 2016-11-11 2020-01-16 エアロバイロメント, インコーポレイテッドAerovironment, Inc. 押出成形された翼の保護システム及び装置
CN107097936B (zh) * 2017-05-05 2023-07-25 深圳市中航电科技有限公司 无人机副翼驱动结构
CN107697272A (zh) * 2017-09-11 2018-02-16 西安冰果智能航空科技有限公司 一种无人机舵面驱动机构
US10773817B1 (en) 2018-03-08 2020-09-15 Northrop Grumman Systems Corporation Bi-directional flow ram air system for an aircraft
JP7096698B2 (ja) * 2018-04-23 2022-07-06 株式会社Subaru 翼構造体、翼構造体の制御方法及び航空機
EP3858728B1 (de) * 2020-01-31 2024-05-01 Goodrich Actuation Systems Limited Klappenbetätigungsanordnung
US11247767B2 (en) * 2020-03-05 2022-02-15 Ruben Leon Wireless autopilot system
US11661175B2 (en) 2020-03-05 2023-05-30 Ruben Leon Wireless autopilot system
EP4124566A1 (de) * 2021-07-27 2023-02-01 Airbus Operations, S.L.U. Bewegliche komponente für flugzeuge
CN117985218B (zh) * 2024-03-21 2024-08-16 中国科学院工程热物理研究所 一种用于飞机机翼的变弯度双模式后缘舵面结构及方法

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Publication number Priority date Publication date Assignee Title
US2670909A (en) 1950-03-01 1954-03-02 Bell Aircraft Corp Actuating mechanism for aircraft extensible flaps
US3109613A (en) 1960-11-28 1963-11-05 Mabel Wilson Raspet Variable-camber airfoil
US3944170A (en) 1974-06-20 1976-03-16 Ltv Aerospace Corporation Apparatus for producing pivotal movement
US4286761A (en) 1978-08-15 1981-09-01 Vought Corporation Eccentric actuator
DE3627219A1 (de) * 1986-08-11 1988-02-18 Eckehart Zehrfeldt Kraftbetaetigtes scharnier mit integrierter auslenkmechanik
US5161757A (en) 1989-07-31 1992-11-10 The Boeing Company Extending bent shaft flap drive
US5222699A (en) 1990-04-16 1993-06-29 Ltv Aerospace And Defense Company Variable control aircraft control surface
US5651513A (en) * 1995-03-01 1997-07-29 Northrop Grumman Corporation Linear flap drive system
US5794893A (en) 1995-06-07 1998-08-18 Northrop Grumman Corporation Elastomeric transition for aircraft control surface
US6244542B1 (en) * 1999-07-20 2001-06-12 Northrop Grumman Corporation Rotor driven edge
US6270039B1 (en) * 1999-10-12 2001-08-07 Patria Finavicomp Oy Hinge for movable control surfaces in an aircraft and a connecting piece to be used with such a hinge

Also Published As

Publication number Publication date
RU2296694C2 (ru) 2007-04-10
IL153055A0 (en) 2003-06-24
EP1316501A3 (de) 2004-04-28
US6467733B1 (en) 2002-10-22
IL153055A (en) 2006-07-05
EP1316501A2 (de) 2003-06-04
EP1316501B1 (de) 2006-06-14
DE60212303T2 (de) 2007-05-16
DE60212303D1 (de) 2006-07-27

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Legal Events

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RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties