FR3102247B1 - Method for determining a defect in a coating covering an aircraft part and aircraft part covered with coating layers - Google Patents

Method for determining a defect in a coating covering an aircraft part and aircraft part covered with coating layers Download PDF

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Publication number
FR3102247B1
FR3102247B1 FR1911631A FR1911631A FR3102247B1 FR 3102247 B1 FR3102247 B1 FR 3102247B1 FR 1911631 A FR1911631 A FR 1911631A FR 1911631 A FR1911631 A FR 1911631A FR 3102247 B1 FR3102247 B1 FR 3102247B1
Authority
FR
France
Prior art keywords
coating
defect
aircraft part
aircraft
determining
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
FR1911631A
Other languages
French (fr)
Other versions
FR3102247A1 (en
Inventor
Romain Chapelle
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 Aircraft Engines SAS
Original Assignee
Safran Aircraft Engines 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 Safran Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1911631A priority Critical patent/FR3102247B1/en
Priority claimed from FR2010141A external-priority patent/FR3102246B1/en
Publication of FR3102247A1 publication Critical patent/FR3102247A1/en
Application granted granted Critical
Publication of FR3102247B1 publication Critical patent/FR3102247B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • 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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288Protective coatings for blades
    • 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
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/005Repairing methods or devices
    • 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
    • G01N21/8422Investigating thin films, e.g. matrix isolation method
    • 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
    • G01N21/8803Visual inspection
    • 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
    • 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
    • F05D2230/00Manufacture
    • F05D2230/90Coating; Surface treatment
    • 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
    • F05D2260/00Function
    • F05D2260/80Diagnostics
    • 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
    • F05D2270/8041Cameras
    • 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
    • F05D2300/00Materials; Properties thereof
    • F05D2300/50Intrinsic material properties or characteristics
    • 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
    • G01N21/8422Investigating thin films, e.g. matrix isolation method
    • G01N2021/8427Coatings
    • 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)
  • Chemical & Material Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Biochemistry (AREA)
  • Mechanical Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • General Physics & Mathematics (AREA)
  • Immunology (AREA)
  • Pathology (AREA)
  • Health & Medical Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Analytical Chemistry (AREA)
  • Materials Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Transportation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mathematical Physics (AREA)
  • Investigating Materials By The Use Of Optical Means Adapted For Particular Applications (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)

Abstract

Procédé de détermination d’un défaut dans un revêtement recouvrant une pièce d’un aéronef et pièce d’aéronef recouverte de couches de revêtement L’invention concerne un procédé de détermination d’un défaut (140) dans un revêtement recouvrant une pièce (100) d’un aéronef, dans lequel ladite pièce est recouverte d’au moins une première couche de revêtement (120) comportant au moins un pigment luminescent produisant, sous une lumière d’un premier spectre, une première couleur et, sous une lumière d’un second spectre, une seconde couleur, distincte de la première couleur, ledit procédé comportant : une opération d’éclairage de la pièce d’aéronef (100), au moyen d’une lampe (200) émettant une lumière du second spectre, et une opération d’observation de ladite pièce d’aéronef (100) pour détecter si une portion de ladite pièce présente une couleur différente de l’ensemble de la pièce, correspondant à un défaut de revêtement. Figure à publier avec l’abrégé : Figure 2Method for determining a defect in a coating covering a part of an aircraft and part of an aircraft covered with coating layers The invention relates to a method for determining a defect (140) in a coating covering a part (100 ) of an aircraft, in which said part is covered with at least a first coating layer (120) comprising at least one luminescent pigment producing, under a light of a first spectrum, a first color and, under a light of a second spectrum, a second color, distinct from the first color, said method comprising: an operation of illuminating the aircraft part (100), by means of a lamp (200) emitting light of the second spectrum, and an observation operation of said aircraft part (100) to detect if a portion of said part has a different color from the whole of the part, corresponding to a coating defect. Figure to be published with abstract: Figure 2

FR1911631A 2019-10-17 2019-10-17 Method for determining a defect in a coating covering an aircraft part and aircraft part covered with coating layers Active FR3102247B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1911631A FR3102247B1 (en) 2019-10-17 2019-10-17 Method for determining a defect in a coating covering an aircraft part and aircraft part covered with coating layers

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
FR1911631A FR3102247B1 (en) 2019-10-17 2019-10-17 Method for determining a defect in a coating covering an aircraft part and aircraft part covered with coating layers
FR1911631 2019-10-17
FR2010141 2020-10-05
FR2010141A FR3102246B1 (en) 2017-01-26 2020-10-05 Method for determining a defect in a coating covering a part of an aircraft and aircraft part covered with coating layers

Related Child Applications (1)

Application Number Title Priority Date Filing Date
FR2010141A Division FR3102246B1 (en) 2017-01-26 2020-10-05 Method for determining a defect in a coating covering a part of an aircraft and aircraft part covered with coating layers

Publications (2)

Publication Number Publication Date
FR3102247A1 FR3102247A1 (en) 2021-04-23
FR3102247B1 true FR3102247B1 (en) 2022-07-22

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Application Number Title Priority Date Filing Date
FR1911631A Active FR3102247B1 (en) 2019-10-17 2019-10-17 Method for determining a defect in a coating covering an aircraft part and aircraft part covered with coating layers

Country Status (1)

Country Link
FR (1) FR3102247B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU2022381719A1 (en) * 2021-11-03 2024-05-23 Prc-Desoto International, Inc. Damage indicating coating system

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4327155A (en) * 1980-12-29 1982-04-27 General Electric Company Coated metal structures and method for making
GB2367826B (en) * 2000-10-03 2003-07-16 Luminous Technologies Ltd Luminescent paint
US9085052B1 (en) * 2011-05-05 2015-07-21 The Boeing Company Structural repair having optical witness and method of monitoring repair performance

Also Published As

Publication number Publication date
FR3102247A1 (en) 2021-04-23

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