WO2017103408A3 - Dispositif de mesure et de contrôle de conformité d'un impact sur une structure - Google Patents

Dispositif de mesure et de contrôle de conformité d'un impact sur une structure Download PDF

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Publication number
WO2017103408A3
WO2017103408A3 PCT/FR2016/053337 FR2016053337W WO2017103408A3 WO 2017103408 A3 WO2017103408 A3 WO 2017103408A3 FR 2016053337 W FR2016053337 W FR 2016053337W WO 2017103408 A3 WO2017103408 A3 WO 2017103408A3
Authority
WO
WIPO (PCT)
Prior art keywords
impact
measurement means
dimensional measurement
hollow lower
compliance monitoring
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.)
Ceased
Application number
PCT/FR2016/053337
Other languages
English (en)
Other versions
WO2017103408A2 (fr
Inventor
Louis LE PINRU
Hubert Voillaume
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 Group SAS
Original Assignee
Airbus Group 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 Group SAS filed Critical Airbus Group SAS
Publication of WO2017103408A2 publication Critical patent/WO2017103408A2/fr
Publication of WO2017103408A3 publication Critical patent/WO2017103408A3/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N21/00Investigating or analysing materials by the use of optical means, i.e. using sub-millimetre waves, infrared, visible or ultraviolet light
    • G01N21/84Systems specially adapted for particular applications
    • G01N21/88Investigating the presence of flaws or contamination
    • G01N21/8806Specially adapted optical and illumination features
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/60Testing or inspecting aircraft components or systems
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00Regulating or controlling by varying flow
    • F01D17/02Arrangement of sensing elements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D17/00Regulating or controlling by varying flow
    • F01D17/20Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D21/00Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
    • F01D21/003Arrangements for testing or measuring
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B11/00Measuring arrangements characterised by the use of optical techniques
    • G01B11/24Measuring arrangements characterised by the use of optical techniques for measuring contours or curvatures
    • G01B11/25Measuring arrangements characterised by the use of optical techniques for measuring contours or curvatures by projecting a pattern, e.g. one or more lines, moiré fringes on the object
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01BMEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B5/00Measuring arrangements characterised by the use of mechanical techniques
    • G01B5/0002Arrangements for supporting, fixing or guiding the measuring instrument or the object to be measured
    • G01B5/0004Supports
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00Control
    • F05D2270/80Devices generating input signals, e.g. transducers, sensors, cameras or strain gauges
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00Control
    • F05D2270/80Devices generating input signals, e.g. transducers, sensors, cameras or strain gauges
    • F05D2270/804Optical devices
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Analytical Chemistry (AREA)
  • Transportation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Health & Medical Sciences (AREA)
  • Computer Vision & Pattern Recognition (AREA)
  • Chemical & Material Sciences (AREA)
  • Manufacturing & Machinery (AREA)
  • Biochemistry (AREA)
  • General Health & Medical Sciences (AREA)
  • Immunology (AREA)
  • Pathology (AREA)
  • Length Measuring Devices By Optical Means (AREA)
  • Force Measurement Appropriate To Specific Purposes (AREA)
  • Investigating Strength Of Materials By Application Of Mechanical Stress (AREA)

Abstract

L'invention est relative à un dispositif (100) de mesure et de contrôle de conformité d'un impact (220) sur une structure (200). Il comporte : - un cadre support (10) comportant une face inférieure creuse (13) destinée à être positionnée, en regard de l'impact, contre une surface (210) de la structure (200), la face inférieure creuse définissant un plan de pose (14), - un moyen de mesure dimensionnelle optique (20) configuré pour être dirigé en direction de la face inférieure creuse (13), ledit moyen de mesure dimensionnelle optique étant positionné sur le cadre support (10) à une distance telle que le plan de pose (14) coïncide avec un plan de référence dudit moyen de mesure dimensionnelle optique, - un module de gestion (30) comportant une unité de traitement d'au moins une image obtenue par le moyen de mesure dimensionnelle optique (20) et un écran de visualisation (31) destiné à délivrer une information relative à la conformité de l'impact.
PCT/FR2016/053337 2015-12-17 2016-12-12 Dispositif de mesure et de contrôle de conformité d'un impact sur une structure Ceased WO2017103408A2 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1562581 2015-12-17
FR1562581A FR3045828B1 (fr) 2015-12-17 2015-12-17 Dispositif de mesure et de controle de conformite d'un impact sur une structure

Publications (2)

Publication Number Publication Date
WO2017103408A2 WO2017103408A2 (fr) 2017-06-22
WO2017103408A3 true WO2017103408A3 (fr) 2017-08-10

Family

ID=55361789

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/FR2016/053337 Ceased WO2017103408A2 (fr) 2015-12-17 2016-12-12 Dispositif de mesure et de contrôle de conformité d'un impact sur une structure

Country Status (2)

Country Link
FR (1) FR3045828B1 (fr)
WO (1) WO2017103408A2 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP4239279B1 (fr) * 2022-03-04 2025-08-20 Airbus Operations GmbH Système et procédé de vérification d'une surface d'un aéronef ou d'un vaisseau spatial

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2685082A3 (en) * 1991-09-07 1993-06-18 Lukassen Flughafentechnik Gmbh Control device for levels of water incorporated in aircraft
US5311286A (en) * 1992-04-01 1994-05-10 Materials Technologies Corporation Apparatus and method for optically measuring a surface
US20040233421A1 (en) * 2001-05-08 2004-11-25 Wolfgang Weinhold Method and device for examining an object in a contactless manner, especially for examining the surface form of the same
EP1580524A2 (fr) * 2004-03-25 2005-09-28 Airbus France Procédé et dispositif de caractérisation d'un endommagement de structure faisant appel au moiré d'ombre
WO2007012781A2 (fr) * 2005-07-26 2007-02-01 Airbus France Procede de mesure d'une anomalie de forme sur un panneau d'une structure d'aeronef et systeme de mise en oeuvre
EP2108921A1 (fr) * 2008-04-11 2009-10-14 Visuol Technologies Dispositif de contrôle de la qualité de surface
WO2015187435A2 (fr) * 2014-06-06 2015-12-10 Faro Technologies, Inc. Système d'instrument de métrologie et procédé de fonctionnement

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2685082A3 (en) * 1991-09-07 1993-06-18 Lukassen Flughafentechnik Gmbh Control device for levels of water incorporated in aircraft
US5311286A (en) * 1992-04-01 1994-05-10 Materials Technologies Corporation Apparatus and method for optically measuring a surface
US20040233421A1 (en) * 2001-05-08 2004-11-25 Wolfgang Weinhold Method and device for examining an object in a contactless manner, especially for examining the surface form of the same
EP1580524A2 (fr) * 2004-03-25 2005-09-28 Airbus France Procédé et dispositif de caractérisation d'un endommagement de structure faisant appel au moiré d'ombre
WO2007012781A2 (fr) * 2005-07-26 2007-02-01 Airbus France Procede de mesure d'une anomalie de forme sur un panneau d'une structure d'aeronef et systeme de mise en oeuvre
EP2108921A1 (fr) * 2008-04-11 2009-10-14 Visuol Technologies Dispositif de contrôle de la qualité de surface
WO2015187435A2 (fr) * 2014-06-06 2015-12-10 Faro Technologies, Inc. Système d'instrument de métrologie et procédé de fonctionnement

Also Published As

Publication number Publication date
FR3045828A1 (fr) 2017-06-23
WO2017103408A2 (fr) 2017-06-22
FR3045828B1 (fr) 2019-04-05

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