ATE380363T1 - 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
ATE380363T1
ATE380363T1 AT05291186T AT05291186T ATE380363T1 AT E380363 T1 ATE380363 T1 AT E380363T1 AT 05291186 T AT05291186 T AT 05291186T AT 05291186 T AT05291186 T AT 05291186T AT E380363 T1 ATE380363 T1 AT E380363T1
Authority
AT
Austria
Prior art keywords
aircraft
rectar
final
twist
load limits
Prior art date
Application number
AT05291186T
Other languages
English (en)
Inventor
Franck Delaplace
Sylvie Marquier
Gerard Mathieu
Gennaro Squeglia
Original Assignee
Airbus France
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 France filed Critical Airbus France
Application granted granted Critical
Publication of ATE380363T1 publication Critical patent/ATE380363T1/de

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)
  • Force Measurement Appropriate To Specific Purposes (AREA)
  • Tires In General (AREA)
  • Traffic Control Systems (AREA)
AT05291186T 2004-06-15 2005-06-02 Verfahren und vorrichtung zur ermittlung eines überschreitens der belastungsgrenzen eines flugzeugseitenleitwerkes ATE380363T1 (de)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
ATE380363T1 true ATE380363T1 (de) 2007-12-15

Family

ID=34942373

Family Applications (1)

Application Number Title Priority Date Filing Date
AT05291186T ATE380363T1 (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
CA3037923C (en) * 2018-03-29 2025-12-09 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
EP1607815B1 (de) 2007-12-05
EP1607815A1 (de) 2005-12-21
US20070136030A1 (en) 2007-06-14
CA2509427A1 (fr) 2005-12-15
DE602005003614T2 (de) 2008-11-13
CA2509427C (fr) 2012-08-07
DE602005003614D1 (de) 2008-01-17
US7271741B2 (en) 2007-09-18
FR2871440A1 (fr) 2005-12-16
FR2871440B1 (fr) 2006-09-08

Similar Documents

Publication Publication Date Title
Ding et al. Fatigue damage evaluation of broad-band Gaussian and non-Gaussian wind load effects by a spectral method
DE602005019734D1 (de) Trennung von ereignis- und störungsparametern
ATE380363T1 (de) Verfahren und vorrichtung zur ermittlung eines überschreitens der belastungsgrenzen eines flugzeugseitenleitwerkes
WO2007124231A3 (en) A method for measuring and improving organization effectiveness
EP2634711A3 (de) System und Verfahren zur Strukturanalyse
EP2237109A3 (de) Verfahren zur Prüfung und Beurteilung eines Photomaskenrohlings oder eines Zwischenprodukts davon
EP2500557A3 (de) Verfahren und Vorrichtung zur Erkennung von Gassensorfehlern
CN103604688A (zh) 一种基于临界面法的塑性金属材料多轴高周疲劳寿命预测方法
EP2390471A3 (de) Schaufelnüberwachungssystem
WO2018087338A3 (de) Inspektionsverfahren und inspektionssystem zum inspizieren eines fahrzeugs im betriebszustand
Casafont et al. Linear buckling analysis of thin-walled members combining the Generalised Beam Theory and the Finite Element Method
CN108918253B (zh) 测量落锤撕裂试验材料真实断裂能的方法
EP2660717A3 (de) Vorrichtung zur Prädikatsberechnung in Prozessorbefehlssatz
Hu et al. A novel size independent symplectic analytical singular element for inclined crack terminating at bimaterial interface
GB2482455A (en) Method for balancing a wind turbine
ATE544107T1 (de) Verfahren zur prognose einer belastungen ausgesetzten struktur
WO2007035834A3 (en) Methods and systems for creating a recipe for a defect review process
EP2957883A3 (de) Verfahren zur prognose einer flugzeugstruktur auf basis von struktureller prüfung
EP2594914A3 (de) System und Verfahren zum Schätzen der Betriebstemperatur einer Turbomaschinerie
ATE380362T1 (de) Verfahren und vorrichtung zur ermittlung eines überschreitens der belastungsgrenzen eines flugzeughöhenleitwerkes
WO2013076579A3 (en) Method for assessing risk of bone fracture
ATE416409T1 (de) Verfahren und vorrichtung zum fliegen eines sich aufbäumenden flugzeugs
SG149739A1 (en) Multi-axis vibration method and apparatus
ATE385327T1 (de) Verfahren und vorrichtung zur ermittlung eines überschreitens der belastungsgrenzen einer flugzeugstruktur
WO2010046299A3 (de) Turbinenschaufelblatt und turbinenschaufel für eine turbine sowie verfahren zur direkten bestimmung des erosionsfortschritts eines turbinenschaufelblattes

Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties