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 PDFInfo
- 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
Links
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
- F01D5/288—Protective coatings for blades
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND 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
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/60—Testing or inspecting aircraft components or systems
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/005—Repairing methods or devices
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N21/00—Investigating or analysing materials by the use of optical means, i.e. using sub-millimetre waves, infrared, visible or ultraviolet light
- G01N21/84—Systems specially adapted for particular applications
- G01N21/8422—Investigating thin films, e.g. matrix isolation method
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N21/00—Investigating or analysing materials by the use of optical means, i.e. using sub-millimetre waves, infrared, visible or ultraviolet light
- G01N21/84—Systems specially adapted for particular applications
- G01N21/88—Investigating the presence of flaws or contamination
- G01N21/8803—Visual inspection
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/003—Arrangements for testing or measuring
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2230/00—Manufacture
- F05D2230/90—Coating; Surface treatment
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/80—Diagnostics
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/80—Devices generating input signals, e.g. transducers, sensors, cameras or strain gauges
- F05D2270/804—Optical devices
- F05D2270/8041—Cameras
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2300/00—Materials; Properties thereof
- F05D2300/50—Intrinsic material properties or characteristics
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N21/00—Investigating or analysing materials by the use of optical means, i.e. using sub-millimetre waves, infrared, visible or ultraviolet light
- G01N21/84—Systems specially adapted for particular applications
- G01N21/8422—Investigating thin films, e.g. matrix isolation method
- G01N2021/8427—Coatings
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- Y—GENERAL 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient 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
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 |
Family
ID=82448755
Family Applications (1)
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)
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)
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 |
-
2019
- 2019-10-17 FR FR1911631A patent/FR3102247B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
FR3102247A1 (en) | 2021-04-23 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 2 |
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PLSC | Publication of the preliminary search report |
Effective date: 20210423 |
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PLFP | Fee payment |
Year of fee payment: 3 |
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PLFP | Fee payment |
Year of fee payment: 4 |
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PLFP | Fee payment |
Year of fee payment: 5 |