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FR3010522B1 - NON-DESTRUCTIVE CONTROL SYSTEM OF A COMPOSITE MATERIAL AND AIRCRAFT COMPRISING SUCH A SYSTEM - Google Patents

NON-DESTRUCTIVE CONTROL SYSTEM OF A COMPOSITE MATERIAL AND AIRCRAFT COMPRISING SUCH A SYSTEM

Info

Publication number
FR3010522B1
FR3010522B1 FR1358574A FR1358574A FR3010522B1 FR 3010522 B1 FR3010522 B1 FR 3010522B1 FR 1358574 A FR1358574 A FR 1358574A FR 1358574 A FR1358574 A FR 1358574A FR 3010522 B1 FR3010522 B1 FR 3010522B1
Authority
FR
France
Prior art keywords
aircraft
composite material
control system
destructive control
destructive
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
FR1358574A
Other languages
French (fr)
Other versions
FR3010522A1 (en
Inventor
Nicolas Cabanac
Alexandre Lestruhaut
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 Operations SAS
Original Assignee
Airbus Operations SAS
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 Operations SAS filed Critical Airbus Operations SAS
Priority to FR1358574A priority Critical patent/FR3010522B1/en
Publication of FR3010522A1 publication Critical patent/FR3010522A1/en
Application granted granted Critical
Publication of FR3010522B1 publication Critical patent/FR3010522B1/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • G01M11/00—Testing of optical apparatus; Testing structures by optical methods not otherwise provided for
    • G01M11/08—Testing mechanical properties
    • G01M11/083—Testing mechanical properties by using an optical fiber in contact with the device under test [DUT]
    • G01M11/086—Details about the embedment of the optical fiber within the DUT
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0033—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by determining damage, crack or wear
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M5/00—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings
    • G01M5/0091—Investigating the elasticity of structures, e.g. deflection of bridges or air-craft wings by using electromagnetic excitation or detection

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Analytical Chemistry (AREA)
  • Electromagnetism (AREA)
  • Length Measuring Devices By Optical Means (AREA)
FR1358574A 2013-09-06 2013-09-06 NON-DESTRUCTIVE CONTROL SYSTEM OF A COMPOSITE MATERIAL AND AIRCRAFT COMPRISING SUCH A SYSTEM Expired - Fee Related FR3010522B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1358574A FR3010522B1 (en) 2013-09-06 2013-09-06 NON-DESTRUCTIVE CONTROL SYSTEM OF A COMPOSITE MATERIAL AND AIRCRAFT COMPRISING SUCH A SYSTEM

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1358574A FR3010522B1 (en) 2013-09-06 2013-09-06 NON-DESTRUCTIVE CONTROL SYSTEM OF A COMPOSITE MATERIAL AND AIRCRAFT COMPRISING SUCH A SYSTEM

Publications (2)

Publication Number Publication Date
FR3010522A1 FR3010522A1 (en) 2015-03-13
FR3010522B1 true FR3010522B1 (en) 2017-04-28

Family

ID=49484335

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1358574A Expired - Fee Related FR3010522B1 (en) 2013-09-06 2013-09-06 NON-DESTRUCTIVE CONTROL SYSTEM OF A COMPOSITE MATERIAL AND AIRCRAFT COMPRISING SUCH A SYSTEM

Country Status (1)

Country Link
FR (1) FR3010522B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP7117993B2 (en) * 2018-12-25 2022-08-15 フクビ化学工業株式会社 FRP pultruded body and manufacturing method thereof

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4581527A (en) * 1983-07-29 1986-04-08 The United States Of America As Represented By The Secretary Of The Navy Damage assessment system for composite plastic structures using fiber optics
US4537469A (en) * 1984-05-25 1985-08-27 Grumman Aerospace Corporation Multi-function composite material utilizing embedded optical fibers
US4836030A (en) * 1985-05-20 1989-06-06 Lockheed Corporation Method of testing composite materials for structural damage
US4936649A (en) * 1989-01-25 1990-06-26 Lymer John D Damage evaluation system and method using optical fibers
US4930852A (en) * 1989-02-21 1990-06-05 Simmonds Precision Product, Inc. Optical fiber mounting and structural monitoring
JPH05138787A (en) * 1991-11-25 1993-06-08 Toyota Autom Loom Works Ltd Laminated composite material
US6486465B1 (en) * 2000-10-10 2002-11-26 Gregory S. Hein Method of detecting flaws in structural members
FR2901608B1 (en) * 2006-05-24 2009-04-03 Airbus France Sas SYSTEM FOR MEASURING AND DETECTING PARAMETERS AND ANOMALIES
WO2008102344A1 (en) * 2007-02-20 2008-08-28 Cyclone Aviation Products Ltd. System and method for embedding an optical fiber layer in layered composite material
DK2112374T4 (en) * 2008-04-21 2019-01-28 Siemens Ag Breakage detection system
DE102008026781A1 (en) * 2008-06-04 2009-12-10 Hardung, Heimo von, Prof. Dr. Component for use in e.g. fuselage, of aircraft, has fiber-reinforced plastic part and fiber e.g. optical glass fiber, for guiding electrical or electromagnetic and/or optical signal such as light signal through component
US20130050685A1 (en) * 2011-08-23 2013-02-28 The Boeing Company Composite structure having an embedded sensing system

Also Published As

Publication number Publication date
FR3010522A1 (en) 2015-03-13

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