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WO2006111679A3 - Procede et dispositif de surveillance d'une structure d'un avion - Google Patents

Procede et dispositif de surveillance d'une structure d'un avion Download PDF

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Publication number
WO2006111679A3
WO2006111679A3 PCT/FR2006/050351 FR2006050351W WO2006111679A3 WO 2006111679 A3 WO2006111679 A3 WO 2006111679A3 FR 2006050351 W FR2006050351 W FR 2006050351W WO 2006111679 A3 WO2006111679 A3 WO 2006111679A3
Authority
WO
WIPO (PCT)
Prior art keywords
aircraft
monitoring
aircraft structure
servicing
critical parts
Prior art date
Application number
PCT/FR2006/050351
Other languages
English (en)
Other versions
WO2006111679A2 (fr
Inventor
Didier Honore Bramban
Original Assignee
Eads Europ Aeronautic Defence
Eads Ccr Groupement D Interet
Didier Honore Bramban
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 Eads Europ Aeronautic Defence, Eads Ccr Groupement D Interet, Didier Honore Bramban filed Critical Eads Europ Aeronautic Defence
Priority to US11/918,810 priority Critical patent/US20110112775A1/en
Priority to JP2008507139A priority patent/JP4745385B2/ja
Priority to CA002605565A priority patent/CA2605565A1/fr
Priority to EP06743809A priority patent/EP1917497A2/fr
Publication of WO2006111679A2 publication Critical patent/WO2006111679A2/fr
Publication of WO2006111679A3 publication Critical patent/WO2006111679A3/fr

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
    • G01N29/04—Analysing solids
    • G01N29/045—Analysing solids by imparting shocks to the workpiece and detecting the vibrations or the acoustic waves caused by the shocks
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B17/00—Measuring arrangements characterised by the use of infrasonic, sonic or ultrasonic vibrations
    • G01B17/04—Measuring arrangements characterised by the use of infrasonic, sonic or ultrasonic vibrations for measuring the deformation in a solid, e.g. by vibrating string
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01H—MEASUREMENT OF MECHANICAL VIBRATIONS OR ULTRASONIC, SONIC OR INFRASONIC WAVES
    • G01H1/00—Measuring characteristics of vibrations in solids by using direct conduction to the detector
    • G01H1/12—Measuring characteristics of vibrations in solids by using direct conduction to the detector of longitudinal or not specified vibrations
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
    • G01N29/22—Details, e.g. general constructional or apparatus details
    • G01N29/24—Probes
    • G01N29/2475—Embedded probes, i.e. probes incorporated in objects to be inspected
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00—Investigating or analysing materials by the use of ultrasonic, sonic or infrasonic waves; Visualisation of the interior of objects by transmitting ultrasonic or sonic waves through the object
    • G01N29/44—Processing the detected response signal, e.g. electronic circuits specially adapted therefor
    • G01N29/46—Processing the detected response signal, e.g. electronic circuits specially adapted therefor by spectral analysis, e.g. Fourier analysis or wavelet analysis
    • G—PHYSICS
    • G07—CHECKING-DEVICES
    • G07C—TIME OR ATTENDANCE REGISTERS; REGISTERING OR INDICATING THE WORKING OF MACHINES; GENERATING RANDOM NUMBERS; VOTING OR LOTTERY APPARATUS; ARRANGEMENTS, SYSTEMS OR APPARATUS FOR CHECKING NOT PROVIDED FOR ELSEWHERE
    • G07C5/00—Registering or indicating the working of vehicles
    • G07C5/08—Registering or indicating performance data other than driving, working, idle, or waiting time, with or without registering driving, working, idle or waiting time
    • G07C5/0808—Diagnosing performance data
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2291/00—Indexing codes associated with group G01N29/00
    • G01N2291/26—Scanned objects
    • G01N2291/269—Various geometry objects
    • G01N2291/2694—Wings or other aircraft parts

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Immunology (AREA)
  • Pathology (AREA)
  • Chemical & Material Sciences (AREA)
  • Analytical Chemistry (AREA)
  • Biochemistry (AREA)
  • General Health & Medical Sciences (AREA)
  • Health & Medical Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Signal Processing (AREA)
  • Acoustics & Sound (AREA)
  • Mathematical Physics (AREA)
  • Spectroscopy & Molecular Physics (AREA)
  • Testing Or Calibration Of Command Recording Devices (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
  • Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)

Abstract

Pour résoudre un problème de maintenance d'un avion, on prévoit de munir cet avion d'un dispositif de surveillance permanente. Ce dispositif comporte des capteurs piézo-électriques. Les signaux délivrés par les capteurs sont enregistrés en permanence. On en déduit à terme la fatigue subie par des parties critiques de l'avion. Ces dernières sont ainsi bien mieux surveillées. On montre qu'on réduit le coût des opérations de maintenance.
PCT/FR2006/050351 2005-04-18 2006-04-14 Procede et dispositif de surveillance d'une structure d'un avion WO2006111679A2 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
US11/918,810 US20110112775A1 (en) 2005-04-18 2006-04-14 Method and device for monitoring an aircraft structure
JP2008507139A JP4745385B2 (ja) 2005-04-18 2006-04-14 飛行機の構造体の監視方法および監視装置
CA002605565A CA2605565A1 (fr) 2005-04-18 2006-04-14 Procede et dispositif de surveillance d'une structure d'un avion
EP06743809A EP1917497A2 (fr) 2005-04-18 2006-04-14 Procede et dispositif de surveillance d'une structure d'un avion

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0550982A FR2884605B1 (fr) 2005-04-18 2005-04-18 Procede et dispositif de surveillance d'une structure d'un avion
FR0550982 2005-04-18

Publications (2)

Publication Number Publication Date
WO2006111679A2 WO2006111679A2 (fr) 2006-10-26
WO2006111679A3 true WO2006111679A3 (fr) 2006-11-30

Family

ID=35466121

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FR2006/050351 WO2006111679A2 (fr) 2005-04-18 2006-04-14 Procede et dispositif de surveillance d'une structure d'un avion

Country Status (7)

Country Link
US (1) US20110112775A1 (fr)
EP (1) EP1917497A2 (fr)
JP (1) JP4745385B2 (fr)
CA (1) CA2605565A1 (fr)
FR (1) FR2884605B1 (fr)
RU (1) RU2385456C2 (fr)
WO (1) WO2006111679A2 (fr)

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US8666569B2 (en) 2007-02-16 2014-03-04 Honeywell International Inc. Methods and systems for health monitoring for aircraft
EP2109839A4 (fr) * 2007-02-16 2013-03-27 Intelligent Automation Corp Système de surveillance de véhicule
EP2063357A1 (fr) * 2007-11-21 2009-05-27 Pepperl + Fuchs Gmbh Support de données transportable et procédé de transmission de données de configuration d'un ordinateur externe vers un capteur
FR2929008B1 (fr) * 2008-03-20 2010-04-02 Eads Europ Aeronautic Defence Dispositif de surveillance de la structure d'un vehicule
FR2932881B1 (fr) 2008-06-19 2010-10-15 Eurocopter France Procede de detection de defaillance d'un capteur analogique et dispositif de detection pour mettre en oeuvre ledit procede
DE102009009189B4 (de) 2009-02-16 2011-06-16 Airbus Operations Gmbh Sensor und Sensornetzwerk für ein Luftfahrzeug
RU2443991C1 (ru) * 2010-07-07 2012-02-27 Сергей Михайлович Мужичек Способ контроля состояния конструкции летательного аппарата и устройство для его осуществления
GB2482124B (en) * 2010-07-19 2016-08-17 Ultra Electronics Ltd Acoustic structural integrity monitoring system and method
US20140142871A1 (en) * 2011-06-28 2014-05-22 International Business Machines Corporation Vibration monitoring system
RU2469289C1 (ru) * 2011-07-13 2012-12-10 Виктор Владимирович Кашковский Устройство контроля прочности крыла воздушного судна
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DE102011055523A1 (de) * 2011-09-09 2013-03-14 Christoph Höweler Verfahren und Vorrichtung zur Schwingungsanalyse von Anlagen oder Maschinenelementen
DE102012000957B4 (de) * 2012-01-19 2021-03-25 Airbus Operations Gmbh Drahtloses Netzwerk mit lokaler Stromversorgung in Flugzeugen
RU2502058C1 (ru) * 2012-08-23 2013-12-20 Сергей Михайлович Мужичек Способ контроля состояния конструкции летательного аппарата и устройство для его осуществления
US9228980B2 (en) 2012-08-29 2016-01-05 Honeywll International Inc. Non-destructive evaluation methods for aerospace components
ITRM20120448A1 (it) * 2012-09-18 2014-03-19 Enea Agenzia Naz Per Le Nuo Ve Tecnologie Strumento per l¿analisi e la misura di segnali provenienti da trasduttori elettrici sensibili all¿intensita¿ di cavitazione o ebollizione di un fluido
US20160047717A1 (en) * 2013-04-05 2016-02-18 Aktiebolaget Skf Method, computer program product & system
US9870690B2 (en) * 2013-10-08 2018-01-16 General Electric Company Methods and systems for a universal wireless platform for asset monitoring
RU2557771C1 (ru) * 2014-02-28 2015-07-27 Закрытое акционерное общество "Научно-производственный центр "Аквамарин" Способ технического контроля и диагностирования бортовых систем беспилотного летательного аппарата с поддержкой принятия решений и комплекс контрольно-проверочной аппаратуры с интеллектуальной системой поддержки принятия решений для его осуществления
RU2545150C1 (ru) * 2014-03-03 2015-03-27 Владимир Иванович Винокуров Способ контроля состояния конструкции летательного аппарата
US9415882B2 (en) * 2014-05-22 2016-08-16 Kidde Technologies, Inc. Overheat sensor system
JP6610987B2 (ja) 2015-02-18 2019-11-27 株式会社Ｉｈｉ 異常診断方法及び異常診断システム
FR3035510B1 (fr) * 2015-04-21 2018-10-26 Airbus Group Sas Moyen acoustique de detection, de localisation et d'evaluation automatique d'impacts subis par une structure
JP6374608B1 (ja) 2016-09-26 2018-08-15 株式会社Ｓｕｂａｒｕ 損傷検知システム及び損傷検知方法
DE102016219931A1 (de) * 2016-10-13 2018-04-19 Airbus Operations Gmbh System und Verfahren zum Entdecken von Radom-Schäden
US11362867B2 (en) 2018-04-17 2022-06-14 University Of Maryland Eastern Shore Systems, methods and apparatus for transmission of data using M-ARY time reversal pulse position modulation
JP2020041814A (ja) 2018-09-06 2020-03-19 株式会社東芝 検知システム、検知方法およびサーバ装置
DE102018131948B4 (de) 2018-12-12 2023-10-26 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren und Vorrichtung zum Detektieren eines Schlagereignisses sowie ein Fahrzeug hierzu
US10728634B2 (en) * 2018-12-19 2020-07-28 Simmonds Precision Products, Inc. Configurable distributed smart sensor system
FR3102977B1 (fr) * 2019-11-07 2021-11-12 Safran Aircraft Engines Dispositif de raccordement de pieces d’un moteur d’aeronef et son procede d’utilisation
CN113155335B (zh) * 2021-02-07 2023-04-07 中北大学 一种两级式微飞片冲击应力测试装置及测试方法
FR3138947A1 (fr) * 2022-08-22 2024-02-23 Ixo Dispositif de detection de rupture de fil(s) dans au moins un cable d’une structure de genie civil

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EP0518508A1 (fr) * 1991-05-24 1992-12-16 Hughes Aircraft Company Système et procédé de localisation de fatique du matériau utilisant des capteurs multiples à émission acoustique
US6170334B1 (en) * 1993-06-25 2001-01-09 Pure Technologies, Ltd. Continuous monitoring of reinforcements in structures
US6192759B1 (en) * 1994-08-31 2001-02-27 Honeywell International Inc. Remote self-powered structure monitor
US20030140701A1 (en) * 2000-06-08 2003-07-31 O'brien Edwin W Method and apparatus for detection of structural damage

Also Published As

Publication number Publication date
CA2605565A1 (fr) 2006-10-26
JP2008536756A (ja) 2008-09-11
RU2007142379A (ru) 2009-05-27
FR2884605B1 (fr) 2007-07-06
FR2884605A1 (fr) 2006-10-20
WO2006111679A2 (fr) 2006-10-26
JP4745385B2 (ja) 2011-08-10
RU2385456C2 (ru) 2010-03-27
EP1917497A2 (fr) 2008-05-07
US20110112775A1 (en) 2011-05-12

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