FR3072459B1 - Procede et dispositif de detection de defauts d'une structure aeronautique - Google Patents

Procede et dispositif de detection de defauts d'une structure aeronautique Download PDF

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Publication number
FR3072459B1
FR3072459B1 FR1759562A FR1759562A FR3072459B1 FR 3072459 B1 FR3072459 B1 FR 3072459B1 FR 1759562 A FR1759562 A FR 1759562A FR 1759562 A FR1759562 A FR 1759562A FR 3072459 B1 FR3072459 B1 FR 3072459B1
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FR
France
Prior art keywords
str
meshes
reception
mesh
excitation
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
FR1759562A
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English (en)
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FR3072459A1 (fr
Inventor
Luca Palladino
Rafik Hadjria
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.)
Safran SA
Commissariat a lEnergie Atomique et aux Energies Alternatives CEA
Original Assignee
Commissariat a lEnergie Atomique CEA
Safran SA
Commissariat a lEnergie Atomique et aux Energies Alternatives CEA
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.)
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Publication date
Application filed by Commissariat a lEnergie Atomique CEA, Safran SA, Commissariat a lEnergie Atomique et aux Energies Alternatives CEA filed Critical Commissariat a lEnergie Atomique CEA
Priority to FR1759562A priority Critical patent/FR3072459B1/fr
Priority to EP18796724.5A priority patent/EP3695219A1/fr
Priority to CN201880077438.6A priority patent/CN111656181B/zh
Priority to US16/755,362 priority patent/US11249050B2/en
Priority to PCT/FR2018/052530 priority patent/WO2019073179A1/fr
Priority to PCT/FR2018/052519 priority patent/WO2019073178A1/fr
Publication of FR3072459A1 publication Critical patent/FR3072459A1/fr
Application granted granted Critical
Publication of FR3072459B1 publication Critical patent/FR3072459B1/fr
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Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00Investigating 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
    • G01N29/04Analysing solids
    • G01N29/041Analysing solids on the surface of the material, e.g. using Lamb, Rayleigh or shear waves
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00Investigating 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
    • G01N29/04Analysing solids
    • G01N29/06Visualisation of the interior, e.g. acoustic microscopy
    • G01N29/0609Display arrangements, e.g. colour displays
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00Investigating 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
    • G01N29/22Details, e.g. general constructional or apparatus details
    • G01N29/223Supports, positioning or alignment in fixed situation
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00Investigating 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
    • G01N29/22Details, e.g. general constructional or apparatus details
    • G01N29/24Probes
    • G01N29/2475Embedded probes, i.e. probes incorporated in objects to be inspected
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00Investigating 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
    • G01N29/44Processing the detected response signal, e.g. electronic circuits specially adapted therefor
    • G01N29/4445Classification of defects
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N29/00Investigating 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
    • G01N29/44Processing the detected response signal, e.g. electronic circuits specially adapted therefor
    • G01N29/4454Signal recognition, e.g. specific values or portions, signal events, signatures
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2291/00Indexing codes associated with group G01N29/00
    • G01N2291/02Indexing codes associated with the analysed material
    • G01N2291/023Solids
    • G01N2291/0231Composite or layered materials
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2291/00Indexing codes associated with group G01N29/00
    • G01N2291/02Indexing codes associated with the analysed material
    • G01N2291/028Material parameters
    • G01N2291/0289Internal structure, e.g. defects, grain size, texture
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2291/00Indexing codes associated with group G01N29/00
    • G01N2291/04Wave modes and trajectories
    • G01N2291/042Wave modes
    • G01N2291/0427Flexural waves, plate waves, e.g. Lamb waves, tuning fork, cantilever
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2291/00Indexing codes associated with group G01N29/00
    • G01N2291/10Number of transducers
    • G01N2291/106Number of transducers one or more transducer arrays
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N2291/00Indexing codes associated with group G01N29/00
    • G01N2291/26Scanned objects
    • G01N2291/269Various geometry objects
    • G01N2291/2694Wings or other aircraft parts

Abstract

L'invention concerne un procédé de détection de défauts d'une structure aéronautique (STR), comprenant les étapes suivantes: • on dispose sur la structure (STR) un maillage constitué d'une pluralité de mailles (M) et défini par une pluralité de transducteurs (100), chaque transducteur étant commandé au moins entre : ○ un mode d'émission dans lequel il est apte à émettre un signal d'excitation vers les autres transducteurs (100), ○ et un mode de réception dans lequel il est apte à recevoir un signal de réception émis par un autre transducteur (100), les signaux d'excitation et de réception étant aptes à se propager à travers la structure (STR), • on extrait, en fonction des signaux d'excitation et de réception, une signature (S) pour chacune des mailles (M), • on compare les signatures (S) entre elles pour identifier parmi les mailles (M) au moins une maille comme localisant un défaut de la structure (STR), appelée maille défaillante, lorsque la signature (S) de cette maille (M) est différente de plusieurs autres signatures (S) de plusieurs autres mailles (M).
FR1759562A 2017-10-12 2017-10-12 Procede et dispositif de detection de defauts d'une structure aeronautique Active FR3072459B1 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
FR1759562A FR3072459B1 (fr) 2017-10-12 2017-10-12 Procede et dispositif de detection de defauts d'une structure aeronautique
EP18796724.5A EP3695219A1 (fr) 2017-10-12 2018-10-11 Dispositif et procédé de détection de défauts d'une structure
CN201880077438.6A CN111656181B (zh) 2017-10-12 2018-10-11 用于检测结构的缺陷的装置和方法
US16/755,362 US11249050B2 (en) 2017-10-12 2018-10-11 Device and method for detecting faults of a structure
PCT/FR2018/052530 WO2019073179A1 (fr) 2017-10-12 2018-10-11 Dispositif et procédé de détection de défauts d'une structure
PCT/FR2018/052519 WO2019073178A1 (fr) 2017-10-12 2018-10-11 Procédé et dispositif de détection de défauts d'une structure aéronautique

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1759562 2017-10-12
FR1759562A FR3072459B1 (fr) 2017-10-12 2017-10-12 Procede et dispositif de detection de defauts d'une structure aeronautique

Publications (2)

Publication Number Publication Date
FR3072459A1 FR3072459A1 (fr) 2019-04-19
FR3072459B1 true FR3072459B1 (fr) 2021-04-23

Family

ID=60765847

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1759562A Active FR3072459B1 (fr) 2017-10-12 2017-10-12 Procede et dispositif de detection de defauts d'une structure aeronautique

Country Status (2)

Country Link
FR (1) FR3072459B1 (fr)
WO (1) WO2019073178A1 (fr)

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7668665B2 (en) * 2003-09-22 2010-02-23 Advanced Structure Monitoring, Inc. Methods of networking interrogation devices for structural conditions
US7647206B2 (en) * 2006-09-15 2010-01-12 The Boeing Company System and method for monitoring structures for damage using nondestructive inspection techniques
US7937248B2 (en) 2007-09-25 2011-05-03 The Boeing Company Virtual time reversal acoustics for structural health monitoring
US8707787B1 (en) * 2011-03-04 2014-04-29 The Boeing Company Time delay based health monitoring system using a sensor network
US20150308920A1 (en) 2014-04-24 2015-10-29 Honeywell International Inc. Adaptive baseline damage detection system and method

Also Published As

Publication number Publication date
WO2019073178A1 (fr) 2019-04-18
FR3072459A1 (fr) 2019-04-19

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