FR2692043B1 - Procede et appareil permettant de soumettre la structure d'un aerodyne a moteur a un essai de secousses en vol. - Google Patents

Procede et appareil permettant de soumettre la structure d'un aerodyne a moteur a un essai de secousses en vol.

Info

Publication number
FR2692043B1
FR2692043B1 FR9306524A FR9306524A FR2692043B1 FR 2692043 B1 FR2692043 B1 FR 2692043B1 FR 9306524 A FR9306524 A FR 9306524A FR 9306524 A FR9306524 A FR 9306524A FR 2692043 B1 FR2692043 B1 FR 2692043B1
Authority
FR
France
Prior art keywords
aerodyne
subjecting
motor
shake test
flight
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
FR9306524A
Other languages
English (en)
Other versions
FR2692043A1 (fr
Inventor
Staple Alan Edward
Wells Daniel Murray
Jordan Andrew Leslie
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.)
AgustaWestland Ltd
Original Assignee
Westland Helicopters Ltd
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 Westland Helicopters Ltd filed Critical Westland Helicopters Ltd
Publication of FR2692043A1 publication Critical patent/FR2692043A1/fr
Application granted granted Critical
Publication of FR2692043B1 publication Critical patent/FR2692043B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M7/00—Vibration-testing of structures; Shock-testing of structures

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
  • Vibration Prevention Devices (AREA)
  • Fuses (AREA)
FR9306524A 1992-06-03 1993-06-01 Procede et appareil permettant de soumettre la structure d'un aerodyne a moteur a un essai de secousses en vol. Expired - Lifetime FR2692043B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB929211719A GB9211719D0 (en) 1992-06-03 1992-06-03 Method & apparatus for in-flight shake testing of an aircraft fuselage

Publications (2)

Publication Number Publication Date
FR2692043A1 FR2692043A1 (fr) 1993-12-10
FR2692043B1 true FR2692043B1 (fr) 1995-08-11

Family

ID=10716444

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9306524A Expired - Lifetime FR2692043B1 (fr) 1992-06-03 1993-06-01 Procede et appareil permettant de soumettre la structure d'un aerodyne a moteur a un essai de secousses en vol.

Country Status (6)

Country Link
US (1) US5390543A (fr)
JP (1) JP3313821B2 (fr)
DE (1) DE4318016B4 (fr)
FR (1) FR2692043B1 (fr)
GB (1) GB9211719D0 (fr)
IT (1) IT1261692B (fr)

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US6229898B1 (en) 1998-12-23 2001-05-08 Sikorsky Aircraft Corporation Active vibration control system using on-line system identification with enhanced noise reduction
US6352220B1 (en) 2000-06-02 2002-03-05 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Helicopter tail boom with venting for alleviation and control of tail boom aerodynamic loads and method thereof
DE10065314B4 (de) * 2000-12-30 2007-08-16 Igus - Innovative Technische Systeme Gmbh Verfahren und Einrichtung zur Überwachung des Zustandes von Rotorblättern an Windkraftanlagen
US6947852B2 (en) * 2002-06-04 2005-09-20 Kla-Tencor Technologies Corporation Monitoring and correcting for non-translational motion in a resonance measurement apparatus
US7966872B2 (en) * 2008-07-23 2011-06-28 The Boeing Company In-flight testing kits and methods for evaluating proposed aerodynamic structures for aircraft
FR2954273B1 (fr) * 2009-12-17 2012-02-24 Eurocopter France Structure porteuse d'un rotor, et appareil volant muni d'une telle structure porteuse
DE102010021026A1 (de) 2010-05-19 2011-11-24 Eads Deutschland Gmbh Hybrides Antriebs- und Energiesystem für Fluggeräte
DE102010021024B4 (de) * 2010-05-19 2014-07-03 Eads Deutschland Gmbh Hauptrotorantrieb für Hubschrauber
KR101239637B1 (ko) * 2011-11-21 2013-03-11 국방과학연구소 비행체의 롤 진동 측정 장치 및 방법
CN106596014B (zh) * 2016-11-29 2019-02-26 中国直升机设计研究所 一种直升机舱内飞行振动环境模拟试验方法
WO2019212606A1 (fr) 2018-04-30 2019-11-07 Lord Corporation Commande de vibrations active de structure et de vibrations de siège
CN109186741A (zh) * 2018-09-30 2019-01-11 华南理工大学 一种非接触式飞机尾翼的振动检测装置与方法
US10633119B1 (en) * 2018-12-05 2020-04-28 The Boeing Company Methods of testing a monument that is to be attached to a floor of an aircraft
CN109765022B (zh) * 2019-01-16 2024-04-16 南京航空航天大学 一种直升机主减速器隔振系统试验装置
CN112213061B (zh) * 2020-09-25 2022-11-04 中国直升机设计研究所 一种用于直升机振动主动控制系统的多向激励装置及系统
CN112498738B (zh) * 2020-12-11 2022-10-18 中国直升机设计研究所 一种直升机飞行控制系统传递特性试验方法
EP4419883A1 (fr) * 2021-10-18 2024-08-28 Jaguar Land Rover Limited Essai de bruit, de vibration et de rudesse pour système d'actionneur électromécanique

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SU1546887A1 (ru) * 1988-06-17 1990-02-28 Vnii Gornoj Geomekhaniki Marks Уctahobka для диhamичeckиx иcпыtahий oбpaзцob matepиaлob пpи cboбoдhыx koлeбahияx
SU1796952A1 (ru) * 1990-09-21 1993-02-23 Yurij A Polevoj Cпocoб bибpaциohhoгo kohtpoля пobpeждehий cилobыx элemehtob abиaциohhыx kohctpуkций
GB9104189D0 (en) * 1991-02-28 1991-06-12 Westland Helicopters Active vibration control systems
WO1993001977A1 (fr) * 1991-07-16 1993-02-04 James Bertram King Syteme de controle d'un avion pendant le vol

Also Published As

Publication number Publication date
FR2692043A1 (fr) 1993-12-10
JP3313821B2 (ja) 2002-08-12
IT1261692B (it) 1996-05-29
DE4318016A1 (de) 1993-12-09
US5390543A (en) 1995-02-21
GB9211719D0 (en) 1992-07-15
ITRM930360A0 (it) 1993-06-01
JPH0643066A (ja) 1994-02-18
ITRM930360A1 (it) 1994-12-01
DE4318016B4 (de) 2006-03-16

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