DE602005003614D1 - Verfahren und Vorrichtung zur Ermittlung eines Überschreitens der Belastungsgrenzen eines Flugzeugseitenleitwerkes - Google Patents

Verfahren und Vorrichtung zur Ermittlung eines Überschreitens der Belastungsgrenzen eines Flugzeugseitenleitwerkes

Info

Publication number
DE602005003614D1
DE602005003614D1 DE602005003614T DE602005003614T DE602005003614D1 DE 602005003614 D1 DE602005003614 D1 DE 602005003614D1 DE 602005003614 T DE602005003614 T DE 602005003614T DE 602005003614 T DE602005003614 T DE 602005003614T DE 602005003614 D1 DE602005003614 D1 DE 602005003614D1
Authority
DE
Germany
Prior art keywords
determining
excess
aircraft
twist
side fin
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.)
Active
Application number
DE602005003614T
Other languages
English (en)
Other versions
DE602005003614T2 (de
Inventor
Franck Delaplace
Sylvie Marquier
Gerard Mathieu
Gennaro Squeglia
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
Publication of DE602005003614D1 publication Critical patent/DE602005003614D1/de
Application granted granted Critical
Publication of DE602005003614T2 publication Critical patent/DE602005003614T2/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00—Arrangements or adaptations of instruments
    • B64D43/02—Arrangements or adaptations of instruments for indicating aircraft speed or stalling conditions
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/60—Testing or inspecting aircraft components or systems

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
  • Regulating Braking Force (AREA)
  • Tires In General (AREA)
  • Force Measurement Appropriate To Specific Purposes (AREA)
  • Traffic Control Systems (AREA)
DE602005003614T 2004-06-15 2005-06-02 Verfahren und Vorrichtung zur Ermittlung eines Überschreitens der Belastungsgrenzen eines Flugzeugseitenleitwerkes Active DE602005003614T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0406456A FR2871440B1 (fr) 2004-06-15 2004-06-15 Procede et dispositif pour detecter un depassement de charges de dimensionnement de la derive d'un avion
FR0406456 2004-06-15

Publications (2)

Publication Number Publication Date
DE602005003614D1 true DE602005003614D1 (de) 2008-01-17
DE602005003614T2 DE602005003614T2 (de) 2008-11-13

Family

ID=34942373

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005003614T Active DE602005003614T2 (de) 2004-06-15 2005-06-02 Verfahren und Vorrichtung zur Ermittlung eines Überschreitens der Belastungsgrenzen eines Flugzeugseitenleitwerkes

Country Status (6)

Country Link
US (1) US7271741B2 (de)
EP (1) EP1607815B1 (de)
AT (1) ATE380363T1 (de)
CA (1) CA2509427C (de)
DE (1) DE602005003614T2 (de)
FR (1) FR2871440B1 (de)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2911202B1 (fr) * 2007-01-05 2009-02-13 Airbus France Sas Procede d'optimisation de panneaux raidis sous contraintes '
US8090485B2 (en) * 2007-11-27 2012-01-03 Embraer S.A. Low-frequency flight control system oscillatory faults prevention via horizontal and vertical tail load monitors
FR2946430B1 (fr) * 2009-06-03 2011-08-26 Airbus France Procede et dispositif pour determiner des charges critiques dues a un tremblement sur une structure d'un avion.
US20110313614A1 (en) * 2010-06-21 2011-12-22 Hinnant Jr Harris O Integrated aeroelasticity measurement for vehicle health management
US8629788B1 (en) * 2010-08-10 2014-01-14 Rockwell Collins, Inc. Sensing, display, and dissemination of detected turbulence
US8949090B2 (en) * 2013-01-28 2015-02-03 The Boeing Company Formation flight control
US9821903B2 (en) 2014-07-14 2017-11-21 The Boeing Company Closed loop control of aircraft control surfaces
US10228692B2 (en) 2017-03-27 2019-03-12 Gulfstream Aerospace Corporation Aircraft flight envelope protection and recovery autopilot
CA3037923A1 (en) * 2018-03-29 2019-09-29 Bombardier Inc. System and method for improving the operation of an aircraft
CN110758768B (zh) * 2019-10-15 2022-07-26 中国直升机设计研究所 一种无轴承旋翼柔性梁刚度试验加载装置

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4302745A (en) * 1980-01-10 1981-11-24 The United States Of America As Represented By The Secretary Of The Air Force Aircraft load factor overload warning system
DE3620888A1 (de) * 1986-06-21 1988-01-14 Messerschmitt Boelkow Blohm Betriebslastenueberwachungseinrichtung fuer luftfahrzeuge
US5359326A (en) * 1993-03-16 1994-10-25 The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration Aircraft maneuver envelope warning system
US5549260A (en) * 1995-01-27 1996-08-27 Dynamic Engineering, Inc. Active control device for aircraft tail buffet alleviation
US6125333A (en) * 1997-11-06 2000-09-26 Northrop Grumman Corporation Building block approach for fatigue spectra generation
US6799463B2 (en) * 2001-11-02 2004-10-05 The Boeing Company Method and system for automated fatigue and structural analysis of an element
FR2850084B1 (fr) * 2003-01-21 2005-12-30 Airbus France Procede et systeme de commande d'une gouverne d'aeronef.

Also Published As

Publication number Publication date
US20070136030A1 (en) 2007-06-14
US7271741B2 (en) 2007-09-18
FR2871440A1 (fr) 2005-12-16
EP1607815B1 (de) 2007-12-05
ATE380363T1 (de) 2007-12-15
CA2509427A1 (fr) 2005-12-15
CA2509427C (fr) 2012-08-07
EP1607815A1 (de) 2005-12-21
DE602005003614T2 (de) 2008-11-13
FR2871440B1 (fr) 2006-09-08

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