FR2878227B1 - Systeme de surveillance d'endommagement d'une pale de rotor d'aeronef a voilure tournante - Google Patents

Systeme de surveillance d'endommagement d'une pale de rotor d'aeronef a voilure tournante

Info

Publication number
FR2878227B1
FR2878227B1 FR0412406A FR0412406A FR2878227B1 FR 2878227 B1 FR2878227 B1 FR 2878227B1 FR 0412406 A FR0412406 A FR 0412406A FR 0412406 A FR0412406 A FR 0412406A FR 2878227 B1 FR2878227 B1 FR 2878227B1
Authority
FR
France
Prior art keywords
monitoring
damage
rotor blade
rotary wing
aircraft air
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 - Fee Related
Application number
FR0412406A
Other languages
English (en)
Other versions
FR2878227A1 (fr
Inventor
Jacques Gaffiero
Jean Patrick Boderlique
Claude Laloi
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 Helicopters SAS
Original Assignee
Eurocopter France SA
Eurocopter SA
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 Eurocopter France SA, Eurocopter SA filed Critical Eurocopter France SA
Priority to FR0412406A priority Critical patent/FR2878227B1/fr
Priority to US11/272,778 priority patent/US7473077B2/en
Publication of FR2878227A1 publication Critical patent/FR2878227A1/fr
Application granted granted Critical
Publication of FR2878227B1 publication Critical patent/FR2878227B1/fr
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/006—Safety devices
    • B64C27/007—Safety devices adapted for detection of blade cracks

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Investigating Or Analyzing Materials By The Use Of Electric Means (AREA)
FR0412406A 2004-11-23 2004-11-23 Systeme de surveillance d'endommagement d'une pale de rotor d'aeronef a voilure tournante Expired - Fee Related FR2878227B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0412406A FR2878227B1 (fr) 2004-11-23 2004-11-23 Systeme de surveillance d'endommagement d'une pale de rotor d'aeronef a voilure tournante
US11/272,778 US7473077B2 (en) 2004-11-23 2005-11-15 System for monitoring damage to a rotor blade of a rotary-wing aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0412406A FR2878227B1 (fr) 2004-11-23 2004-11-23 Systeme de surveillance d'endommagement d'une pale de rotor d'aeronef a voilure tournante

Publications (2)

Publication Number Publication Date
FR2878227A1 FR2878227A1 (fr) 2006-05-26
FR2878227B1 true FR2878227B1 (fr) 2008-05-23

Family

ID=34952537

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0412406A Expired - Fee Related FR2878227B1 (fr) 2004-11-23 2004-11-23 Systeme de surveillance d'endommagement d'une pale de rotor d'aeronef a voilure tournante

Country Status (2)

Country Link
US (1) US7473077B2 (fr)
FR (1) FR2878227B1 (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7861592B2 (en) * 2007-02-27 2011-01-04 Siemens Energy, Inc. Blade shroud vibration monitor
US8384605B2 (en) * 2009-02-25 2013-02-26 Sikorsky Aircraft Corporation Wireless communication between a rotating frame of reference and a non-rotating frame of reference
US8886388B2 (en) * 2009-06-29 2014-11-11 The Boeing Company Embedded damage detection system for composite materials of an aircraft
EP2528046A1 (fr) * 2011-05-23 2012-11-28 Ettlin Aktiengesellschaft Dispositif d'alerte et son procédé de fabrication et de fonctionnement
US9234743B2 (en) 2014-01-16 2016-01-12 Sikorsky Aircraft Corporation Tip clearance measurement
JP6189344B2 (ja) * 2015-01-14 2017-08-30 東芝テック株式会社 クラックセンサおよびクラック監視装置
US20190107380A1 (en) * 2017-10-11 2019-04-11 Sikorsky Aircraft Corporation Strain measurement assembly
WO2021165148A1 (fr) * 2020-02-21 2021-08-26 Basf Se Feuille de capteur, matériau composite et système de détection pour détection de dommages d'un matériau composite
US20220009613A1 (en) * 2020-07-10 2022-01-13 Aerion Intellectual Property Management Corporation Aircraft body section with multilayer electrically conductive structure and methods of fabrication

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3596269A (en) 1968-10-25 1971-07-27 Richard H Laska Structural defect monitoring device
FR2119182A5 (fr) 1970-12-23 1972-08-04 Aerospatiale
US3910105A (en) * 1974-08-16 1975-10-07 Boeing Co Method for detection of flaws in composite fiberglass structures
US4106332A (en) * 1977-04-04 1978-08-15 Textron, Inc. Recording monitor for structure faults
US4524620A (en) 1983-02-07 1985-06-25 Hughes Helicopters, Inc. In-flight monitoring of composite structural components such as helicopter rotor blades
BR8907407A (pt) * 1989-02-28 1991-04-16 Inst Elektroswarki Patona Dispositivo para determinar parametros de propagacao de rachaduras de superficie
US5015842A (en) * 1989-06-01 1991-05-14 United Technologies Corporation High density fiber optic damage detection system
US5227731A (en) * 1991-05-24 1993-07-13 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method of continuously determining crack length
US5379644A (en) * 1991-08-15 1995-01-10 Shimizu Costruction Co., Ltd. Strain or stress gauge and method for detecting strain or stress of structure using the same, and plastic composite material for foreknowing progress of breakdown of structure and method using the same
FR2699499B1 (fr) 1992-12-23 1995-03-10 Eurocopter France Pale en composite thermoplastique, notamment pour rotor arrière caréné d'hélicoptère, et son procédé de fabrication avec étape d'injection.
FR2699498B1 (fr) 1992-12-23 1995-03-10 Eurocopter France Pale en composite thermoplastique, notamment pour rotor arrière caréné d'hélicoptère, et son procédé de fabrication.
FR2740379B1 (fr) 1995-10-30 1998-01-02 Eurocopter France Procede de fabrication d'une pale en materiau composite pour rotor d'helicoptere, et pale pouvant etre obtenue par un tel procede
US5952836A (en) * 1997-04-28 1999-09-14 Mcdonnell Douglas Corporation Device and method for detecting workpiece fractures
US7106215B2 (en) * 2004-02-10 2006-09-12 Marishak Jr Frank Ted Device for monitoring the integrity of spacecraft thermal protection tiles

Also Published As

Publication number Publication date
US7473077B2 (en) 2009-01-06
FR2878227A1 (fr) 2006-05-26
US20060239818A1 (en) 2006-10-26

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Legal Events

Date Code Title Description
CD Change of name or company name

Owner name: AIRBUS HELICOPTERS, FR

Effective date: 20140602

PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

Year of fee payment: 13

PLFP Fee payment

Year of fee payment: 14

PLFP Fee payment

Year of fee payment: 15

ST Notification of lapse

Effective date: 20200906