DE60011267D1 - Betätigungssystem für flugsteuerung und anderen funktionen in der luft- und raumfahrt - Google Patents

Betätigungssystem für flugsteuerung und anderen funktionen in der luft- und raumfahrt

Info

Publication number
DE60011267D1
DE60011267D1 DE60011267T DE60011267T DE60011267D1 DE 60011267 D1 DE60011267 D1 DE 60011267D1 DE 60011267 T DE60011267 T DE 60011267T DE 60011267 T DE60011267 T DE 60011267T DE 60011267 D1 DE60011267 D1 DE 60011267D1
Authority
DE
Germany
Prior art keywords
aviation
functions
space
flight control
actuating system
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 - Lifetime
Application number
DE60011267T
Other languages
English (en)
Other versions
DE60011267T2 (de
Inventor
Edward Uttley
William Chambers
Nigel Blackwell
Brian Weller
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.)
BAE Systems PLC
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
Application filed by BAE Systems PLC filed Critical BAE Systems PLC
Application granted granted Critical
Publication of DE60011267D1 publication Critical patent/DE60011267D1/de
Publication of DE60011267T2 publication Critical patent/DE60011267T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/10—Adjustable control surfaces or members, e.g. rudders one surface adjusted by movement of another, e.g. servo tabs

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
  • Mechanical Control Devices (AREA)
  • Fluid-Pressure Circuits (AREA)
  • Toys (AREA)
  • Feedback Control In General (AREA)
DE60011267T 1999-08-03 2000-07-31 Betätigungssystem für flugsteuerung und anderen funktionen in der luft- und raumfahrt Expired - Lifetime DE60011267T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB9918289 1999-08-03
GBGB9918289.1A GB9918289D0 (en) 1999-08-03 1999-08-03 Actuator system for aerospace controls and functions
PCT/GB2000/002943 WO2001008971A1 (en) 1999-08-03 2000-07-31 Actuator system for aerospace controls and functions

Publications (2)

Publication Number Publication Date
DE60011267D1 true DE60011267D1 (de) 2004-07-08
DE60011267T2 DE60011267T2 (de) 2004-09-23

Family

ID=10858507

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60011267T Expired - Lifetime DE60011267T2 (de) 1999-08-03 2000-07-31 Betätigungssystem für flugsteuerung und anderen funktionen in der luft- und raumfahrt

Country Status (8)

Country Link
US (1) US6349900B1 (de)
EP (1) EP1198383B1 (de)
JP (1) JP2003506254A (de)
AU (1) AU6301700A (de)
DE (1) DE60011267T2 (de)
ES (1) ES2216925T3 (de)
GB (1) GB9918289D0 (de)
WO (1) WO2001008971A1 (de)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10116479C2 (de) * 2001-04-03 2003-12-11 Eurocopter Deutschland Verfahren und Regeleinrichtung zur Verstellung einer im Rotorblatt eines Hubschraubers schwenkbar gelagerten Klappe
US6700345B2 (en) * 2001-11-09 2004-03-02 Honeywell Inc. Position sensor and actuating system
FR2853094B1 (fr) * 2003-03-26 2005-05-27 Airbus France Procede pour contrer les vibrations induites dans un aeronef par le fonctionnement en moulinet d'une soufflante et systeme de commandes de vol electriques mettant en oeuvre ce procede
US6827311B2 (en) * 2003-04-07 2004-12-07 Honeywell International, Inc. Flight control actuation system
US8942882B2 (en) 2004-07-02 2015-01-27 The Boeing Company Vehicle health management systems and methods
US7770842B2 (en) * 2004-08-24 2010-08-10 Honeywell International Inc. Aircraft flight control surface actuation system communication architecture
US20070007385A1 (en) * 2005-06-27 2007-01-11 Honeywell International, Inc. Electric flight control surface actuation system electronic architecture
US7549605B2 (en) * 2005-06-27 2009-06-23 Honeywell International Inc. Electric flight control surface actuation system for aircraft flaps and slats
US9340278B2 (en) * 2006-05-17 2016-05-17 Textron Innovations, Inc. Flight control system
US20090302173A1 (en) * 2006-09-01 2009-12-10 Science Applications International Corporation Automatic flight control systems
US8876063B2 (en) * 2007-12-10 2014-11-04 The Boeing Company Flight control using multiple actuators on primary control surfaces with tabs
DE102008022092A1 (de) * 2008-05-05 2009-11-19 Airbus Deutschland Gmbh Fehlertolerantes Stellsystem zur Verstellung von Klappen eines Flugzeugs mit einer Verstell-Kinematik mit feststehender Drehachse
DE102009002435A1 (de) * 2009-04-16 2010-10-21 Airbus Deutschland Gmbh Hochauftriebssystem für ein Flugzeug und Verfahren zum Detektieren von Fehlern in einem Hochauftriebssystem für ein Flugzeug
US20140061370A1 (en) * 2011-02-17 2014-03-06 George L. Vojtech Airship and a Method for Controlling the Airship
US20130009017A1 (en) * 2011-07-06 2013-01-10 Eaton Corporation Electronically synchronized flap system
US9193407B2 (en) 2012-08-21 2015-11-24 John Austin Muth Active downforce generation for a tilting vehicle
US9180961B2 (en) 2013-01-28 2015-11-10 The Boeing Company Control surface for creating variable camber along a wing
US10400680B2 (en) 2016-09-28 2019-09-03 General Electric Company System and method for synchronizing the operation of airfoil actuators of a gas turbine engine
US11787528B2 (en) 2020-12-23 2023-10-17 Whippany Actuation Systems Llc Jam free dual-redundant actuator lane changer system and process

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2733879A (en) * 1956-02-07 noxon
FR1069933A (de) * 1954-07-13
US2568719A (en) * 1947-04-09 1951-09-25 Sperry Corp Control system for aircraft control surface and tab
US2949259A (en) * 1953-08-25 1960-08-16 Bendix Aviat Corp Automatic steering system for aircraft
US2853256A (en) * 1954-08-23 1958-09-23 Boeing Co Internal resistance plate for aircraft control surfaces
US4079902A (en) * 1977-04-18 1978-03-21 Vyacheslav Fedorovich Ryzhko Aircraft control surface actuator
US4124180A (en) 1977-09-08 1978-11-07 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Free wing assembly for an aircraft
US4676460A (en) * 1984-11-28 1987-06-30 The Boeing Company Longitudinal stability augmentation system and method
US4648569A (en) 1985-10-23 1987-03-10 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Airplane automatic control force trimming device for asymmetric engine failures
JP2879946B2 (ja) * 1990-06-04 1999-04-05 帝人製機株式会社 航空機翼のフラッタ抑制システム
FR2672028B1 (fr) * 1991-01-29 1993-05-14 Aerospatiale Systeme permettant d'ameliorer le comportement en flottement d'un aeronef.
US5366176A (en) 1993-04-16 1994-11-22 United Technologies Corp. Feedback-stabilized aerodynamically overbalanced lifting/control surface for aircraft
FR2748720B1 (fr) * 1996-05-17 1998-07-24 Aerospatiale Systeme pour la commande d'un volet compensateur de gouverne d'aeronef

Also Published As

Publication number Publication date
ES2216925T3 (es) 2004-11-01
US6349900B1 (en) 2002-02-26
DE60011267T2 (de) 2004-09-23
WO2001008971A1 (en) 2001-02-08
JP2003506254A (ja) 2003-02-18
EP1198383A1 (de) 2002-04-24
GB9918289D0 (en) 2000-05-24
AU6301700A (en) 2001-02-19
EP1198383B1 (de) 2004-06-02

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Legal Events

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