DE69913602D1 - Flugzeug mit verminderter Flügelbelastung - Google Patents

Flugzeug mit verminderter Flügelbelastung

Info

Publication number
DE69913602D1
DE69913602D1 DE69913602T DE69913602T DE69913602D1 DE 69913602 D1 DE69913602 D1 DE 69913602D1 DE 69913602 T DE69913602 T DE 69913602T DE 69913602 T DE69913602 T DE 69913602T DE 69913602 D1 DE69913602 D1 DE 69913602D1
Authority
DE
Germany
Prior art keywords
aircraft
wing load
reduced wing
reduced
load
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
DE69913602T
Other languages
English (en)
Other versions
DE69913602T2 (de
Inventor
Thierry Bilange
Marie-Laure Divouz-Plantaz
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
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 Airbus Operations SAS filed Critical Airbus Operations SAS
Application granted granted Critical
Publication of DE69913602D1 publication Critical patent/DE69913602D1/de
Publication of DE69913602T2 publication Critical patent/DE69913602T2/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
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02—Initiating means
    • B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0066—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for limitation of acceleration or stress

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Feedback Control In General (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Handcart (AREA)
DE69913602T 1998-04-29 1999-04-16 Flugzeug mit verminderter Flügelbelastung Expired - Lifetime DE69913602T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9805400 1998-04-29
FR9805400A FR2778163B1 (fr) 1998-04-29 1998-04-29 Aeronef a efforts de voilure diminues

Publications (2)

Publication Number Publication Date
DE69913602D1 true DE69913602D1 (de) 2004-01-29
DE69913602T2 DE69913602T2 (de) 2004-12-23

Family

ID=9525830

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69913602T Expired - Lifetime DE69913602T2 (de) 1998-04-29 1999-04-16 Flugzeug mit verminderter Flügelbelastung

Country Status (5)

Country Link
US (1) US6064923A (de)
EP (1) EP0953504B1 (de)
CA (1) CA2270752C (de)
DE (1) DE69913602T2 (de)
FR (1) FR2778163B1 (de)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6915989B2 (en) * 2002-05-01 2005-07-12 The Boeing Company Aircraft multi-axis modal suppression system
CA2444560C (en) * 2002-10-21 2008-09-23 The Boeing Company Method and apparatus for rotatably supporting movable components, including canards
JP4490963B2 (ja) 2003-02-15 2010-06-30 ガルフストリーム・エアロスペース・コーポレイション 航空機キャビン大気組成制御方法
US20050045764A1 (en) * 2003-08-29 2005-03-03 Supersonic Aerospace International, Llc Canard position and dihedral for boom reduction and pitch/directional control
DE60330869D1 (de) * 2003-11-03 2010-02-25 Boeing Co System zur Modenunterdrückung auf mehreren Achsen eines Flugzeugs
US7367530B2 (en) * 2005-06-21 2008-05-06 The Boeing Company Aerospace vehicle yaw generating systems and associated methods
DE102005058081B9 (de) * 2005-12-06 2009-01-29 Airbus Deutschland Gmbh Verfahren zur Rekonstruktion von Böen und Strukturlasten bei Flugzeugen, insbesondere Verkehrsflugzeugen
US7878461B2 (en) * 2006-01-17 2011-02-01 Gulfstream Aerospace Corporation System and method for an integrated backup control system
CA2637226A1 (en) * 2006-01-17 2007-07-26 Gulfstream Aerospace Corporation Apparatus and method for backup control in a distributed flight control system
RU2503585C1 (ru) * 2012-05-21 2014-01-10 Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Уфимский государственный авиационный технический университет" Система автоматического управления углом курса и ограничения нормальной перегрузки летательного аппарата
US9878776B2 (en) * 2014-05-15 2018-01-30 The Boeing Company System and method for optimizing horizontal tail loads
EP3643605B1 (de) 2018-10-25 2022-08-17 Bombardier Inc. System und verfahren zur verringerung der auswirkung einer erregung eines strukturellen flexiblen modus eines flugzeugs
CN109823514B (zh) * 2019-02-02 2021-01-12 北京航空航天大学 一种可调节安装角的易拆卸尾翼结构

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2906889C2 (de) 1979-02-22 1986-06-26 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Flugzeug mit vor und hinter dem Schwerpunkt angeordneten Steuerflächen
US4723214A (en) 1985-02-15 1988-02-02 Grumman Aerospace Corporation Automatic camber control
US4697768A (en) * 1985-11-12 1987-10-06 Grumman Aerospace Corporation Flight control system employing complementary filter
FR2656585B1 (fr) 1989-12-28 1995-01-13 Aerospatiale Systeme pour diminuer les efforts appliques a la voilure et notamment a l'emplanture des ailes d'un aeronef en vol.
US5056027A (en) * 1990-02-26 1991-10-08 Honeywell Inc. Apparatus and method for a smooth transition between calibrated airspeed control of an aircraft and mach number control of an aircraft
US5079711A (en) * 1990-02-26 1992-01-07 The Boeing Company Aircraft high altitude vertical flight path and speed control system
FR2719548B1 (fr) 1994-05-03 1996-07-05 Aerospatiale Avion de transport à empennage avant.

Also Published As

Publication number Publication date
FR2778163B1 (fr) 2000-06-23
CA2270752C (fr) 2005-10-18
EP0953504B1 (de) 2003-12-17
DE69913602T2 (de) 2004-12-23
US6064923A (en) 2000-05-16
FR2778163A1 (fr) 1999-11-05
CA2270752A1 (fr) 1999-10-29
EP0953504A1 (de) 1999-11-03

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Legal Events

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8364 No opposition during term of opposition