EP3184180B1 - Local repair or remanufacture of polymeric erosion coatings - Google Patents
Local repair or remanufacture of polymeric erosion coatings Download PDFInfo
- Publication number
- EP3184180B1 EP3184180B1 EP16204712.0A EP16204712A EP3184180B1 EP 3184180 B1 EP3184180 B1 EP 3184180B1 EP 16204712 A EP16204712 A EP 16204712A EP 3184180 B1 EP3184180 B1 EP 3184180B1
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- EP
- European Patent Office
- Prior art keywords
- erosion coating
- component
- substrate
- recited
- layer
- 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.)
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Links
- 238000000576 coating method Methods 0.000 title claims description 38
- 230000003628 erosive effect Effects 0.000 title claims description 32
- 230000008439 repair process Effects 0.000 title claims description 15
- 239000011248 coating agent Substances 0.000 claims description 33
- 239000000758 substrate Substances 0.000 claims description 19
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 12
- 229910052782 aluminium Inorganic materials 0.000 claims description 12
- 230000007797 corrosion Effects 0.000 claims description 12
- 238000005260 corrosion Methods 0.000 claims description 12
- 239000004593 Epoxy Substances 0.000 claims description 11
- 239000003973 paint Substances 0.000 claims description 10
- 230000002401 inhibitory effect Effects 0.000 claims description 9
- 229920002635 polyurethane Polymers 0.000 claims description 8
- 239000004814 polyurethane Substances 0.000 claims description 8
- 238000000034 method Methods 0.000 claims description 7
- NBIIXXVUZAFLBC-UHFFFAOYSA-N Phosphoric acid Chemical compound OP(O)(O)=O NBIIXXVUZAFLBC-UHFFFAOYSA-N 0.000 claims description 6
- 229910000147 aluminium phosphate Inorganic materials 0.000 claims description 3
- 238000004140 cleaning Methods 0.000 claims 1
- 239000000463 material Substances 0.000 description 3
- CSCPPACGZOOCGX-UHFFFAOYSA-N Acetone Chemical compound CC(C)=O CSCPPACGZOOCGX-UHFFFAOYSA-N 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 239000004215 Carbon black (E152) Substances 0.000 description 1
- JOYRKODLDBILNP-UHFFFAOYSA-N Ethyl urethane Chemical compound CCOC(N)=O JOYRKODLDBILNP-UHFFFAOYSA-N 0.000 description 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 1
- 229920006311 Urethane elastomer Polymers 0.000 description 1
- 239000000567 combustion gas Substances 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 229920001973 fluoroelastomer Polymers 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 229930195733 hydrocarbon Natural products 0.000 description 1
- 150000002430 hydrocarbons Chemical class 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000003607 modifier Substances 0.000 description 1
- TWNQGVIAIRXVLR-UHFFFAOYSA-N oxo(oxoalumanyloxy)alumane Chemical compound O=[Al]O[Al]=O TWNQGVIAIRXVLR-UHFFFAOYSA-N 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000008458 response to injury Effects 0.000 description 1
- 229910052719 titanium Inorganic materials 0.000 description 1
- 239000010936 titanium Substances 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D5/00—Processes for applying liquids or other fluent materials to surfaces to obtain special surface effects, finishes or structures
- B05D5/005—Repairing damaged coatings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D2202/00—Metallic substrate
- B05D2202/20—Metallic substrate based on light metals
- B05D2202/25—Metallic substrate based on light metals based on Al
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D2601/00—Inorganic fillers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B05—SPRAYING OR ATOMISING IN GENERAL; APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D—PROCESSES FOR APPLYING FLUENT MATERIALS TO SURFACES, IN GENERAL
- B05D7/00—Processes, other than flocking, specially adapted for applying liquids or other fluent materials to particular surfaces or for applying particular liquids or other fluent materials
- B05D7/50—Multilayers
- B05D7/52—Two layers
- B05D7/54—No clear coat specified
-
- 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
-
- 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
-
- 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
- F05D2230/80—Repairing, retrofitting or upgrading methods
Definitions
- the present disclosure relates generally to a remanufactures process and, more particularly, to a repair process for aluminum fan blades.
- Gas turbine engines such as those that power modern commercial and military aircraft, generally include a fan section, a compressor section to pressurize an airflow, a combustor section to burn a hydrocarbon fuel in the presence of the pressurized air, and a turbine section to extract energy from the resultant combustion gases.
- the fan section often includes aluminum fan blades designed with a multi-layer polyurethane erosion coating to protect both sides of the airfoil from operational erosion and subsequent corrosion.
- the erosion coatings sustain erosion, FOD and local damage in service, but there is only minimal repair capability for these coatings.
- a method according to one aspect of the present invention is defined in claim 1.
- a corresponding component with a local repair to a multi-layered polyurethane erosion coating according to another aspect of the present invention is defined in claim 5.
- Preferred embodiments are referred to in the dependent claims.
- Figure 1 schematically illustrates a general perspective view of an exemplary component 20, e.g., a fan blade with a multi-layer erosion coating system for a gas turbine engine.
- a component 20 e.g., a fan blade with a multi-layer erosion coating system for a gas turbine engine.
- FIG. 1 schematically illustrates a general perspective view of an exemplary component 20, e.g., a fan blade with a multi-layer erosion coating system for a gas turbine engine.
- a component type is illustrated in the disclosed non-limiting embodiment, other components with a multi-layer erosion coating system such as a part in the airstream of the engine with an erosion resistant coating, more specifically an airfoil, and even more specifically, a guide vane or a fan blade will also benefit herefrom.
- a cross-section of the component 20 is illustrated for an aluminum substrate 30 such as a 2000, 6000, or 7000 series aluminum with a multi-layer coating 35.
- the coating 35 includes a phosphoric acid anodize layer 40, a corrosion inhibiting epoxy bond primer 50, a corrosion inhibiting paint primer 60, and an elastomeric erosion coating 70 such as a urethane or fluoroelastomer as the outer layer. It should be appreciated that various materials may be utilized in accords with this layer structure.
- a local repair 100 for the component 20 is performed on an airflow surface. That is, the local repair of damage is performed in response to damage into the erosion coating system 35 and as deep as the aluminum substrate 30.
- the local repair 100 may be initiated by abrading thru some or all layers in the erosion coating system and may be as deep as the aluminum substrate 30 or for damage that has reached down to the aluminum substrate 30.
- the erosion coating system adjacent to the damage may be abraded, feathered or otherwise prepared and cleaned with, for example aluminum oxide and an acetone wipe to provide for adhesion of the repair coating system .
- the corrosion inhibiting paint primer 60 provides corrosion protection to the aluminum substrate 30 and also facilitates receipt of a filled epoxy paste 200 such as Duralco 4525 manufactured by Cotronics Corp., of Brooklyn NY USA. It is recognized that for other composite or metallic substrates, the paint primer may not need to provide corrosion protection to the substrate and the use of the primer layer may be optional or a non-corrosion inhibiting primer may be utilized.
- the epoxy paste provides for relatively faster thickness build rates than elastomeric coating material options facilitating faster overall repair process times.
- the filled epoxy paste 200 may then be sanded or otherwise finished to provide an acceptable flowpath surface.
- the filled epoxy paste 200 facilitates field repairs, provides erosion protection and protects primer layers within the repair coating system.
Landscapes
- Structures Of Non-Positive Displacement Pumps (AREA)
Description
- The present disclosure relates generally to a remanufactures process and, more particularly, to a repair process for aluminum fan blades.
- Gas turbine engines, such as those that power modern commercial and military aircraft, generally include a fan section, a compressor section to pressurize an airflow, a combustor section to burn a hydrocarbon fuel in the presence of the pressurized air, and a turbine section to extract energy from the resultant combustion gases.
- The fan section often includes aluminum fan blades designed with a multi-layer polyurethane erosion coating to protect both sides of the airfoil from operational erosion and subsequent corrosion. The erosion coatings sustain erosion, FOD and local damage in service, but there is only minimal repair capability for these coatings.
- Methods of locally repairing multi-layered erosion coatings are known from
US 6,171,704 B1 andUS 2005/0019589 . Therein multi-layered coatings are repaired by applying a filled epoxy paste without the prior application of a paint primer in the damaged areas. - A method according to one aspect of the present invention is defined in claim 1. A corresponding component with a local repair to a multi-layered polyurethane erosion coating according to another aspect of the present invention is defined in claim 5. Preferred embodiments are referred to in the dependent claims.
- The foregoing features and elements may be combined in various combinations without exclusivity, unless expressly indicated otherwise. These features and elements as well as the operation of the invention will become more apparent in light of the following description and the accompanying drawings. It should be understood, however, the following description and drawings are intended to be exemplary in nature and non-limiting.
- Various features will become apparent to those skilled in the art from the following detailed description of the disclosed non-limiting embodiment. The drawings that accompany the detailed description can be briefly described as follows:
-
Figure 1 is a general schematic view of an exemplary component as a representative workpiece; -
Figure 2 is an expanded cross section of the component illustrating the OEM coating system; and -
Figure 3 is an expanded cross section of a repair to the component illustrating the repair coating system -
Figure 1 schematically illustrates a general perspective view of anexemplary component 20, e.g., a fan blade with a multi-layer erosion coating system for a gas turbine engine. It should be appreciated that although a particular component type is illustrated in the disclosed non-limiting embodiment, other components with a multi-layer erosion coating system such as a part in the airstream of the engine with an erosion resistant coating, more specifically an airfoil, and even more specifically, a guide vane or a fan blade will also benefit herefrom. - With reference to
Figure 2 , a cross-section of thecomponent 20 is illustrated for analuminum substrate 30 such as a 2000, 6000, or 7000 series aluminum with amulti-layer coating 35. It should be appreciated other materials such as titanium may be provided. Thecoating 35 includes a phosphoricacid anodize layer 40, a corrosion inhibitingepoxy bond primer 50, a corrosion inhibitingpaint primer 60, and anelastomeric erosion coating 70 such as a urethane or fluoroelastomer as the outer layer. It should be appreciated that various materials may be utilized in accords with this layer structure. - With reference to
Figure 3 , alocal repair 100 for thecomponent 20 is performed on an airflow surface. That is, the local repair of damage is performed in response to damage into theerosion coating system 35 and as deep as thealuminum substrate 30. Thelocal repair 100 may be initiated by abrading thru some or all layers in the erosion coating system and may be as deep as thealuminum substrate 30 or for damage that has reached down to thealuminum substrate 30. The erosion coating system adjacent to the damage may be abraded, feathered or otherwise prepared and cleaned with, for example aluminum oxide and an acetone wipe to provide for adhesion of the repair coating system . - Next, the corrosion inhibiting
paint primer 60 is applied over thealuminum substrate 30. The corrosion inhibitingpaint primer 60 provide corrosion protection to thealuminum substrate 30 and also facilitates receipt of a filledepoxy paste 200 such as Duralco 4525 manufactured by Cotronics Corp., of Brooklyn NY USA. It is recognized that for other composite or metallic substrates, the paint primer may not need to provide corrosion protection to the substrate and the use of the primer layer may be optional or a non-corrosion inhibiting primer may be utilized. The epoxy paste provides for relatively faster thickness build rates than elastomeric coating material options facilitating faster overall repair process times. The filledepoxy paste 200 may then be sanded or otherwise finished to provide an acceptable flowpath surface. - The filled
epoxy paste 200 facilitates field repairs, provides erosion protection and protects primer layers within the repair coating system. - The use of the terms "a," "an," "the," and similar references in the context of description (especially in the context of the following claims) are to be construed to cover both the singular and the plural, unless otherwise indicated herein or specifically contradicted by context. The modifier "about" used in connection with a quantity is inclusive of the stated value and has the meaning dictated by the context (e.g., it includes the degree of error associated with measurement of the particular quantity). All ranges disclosed herein are inclusive of the endpoints, and the endpoints are independently combinable with each other. It should be appreciated that relative positional terms such as "forward," "aft," "upper," "lower," "above," "below," and the like are with reference to the normal operational attitude of the vehicle and should not be considered otherwise limiting.
- Although the different non-limiting embodiments have specific illustrated components, the embodiments of this invention are not limited to those particular combinations. It is possible to use some of the components or features from any of the non-limiting embodiments in combination with features or components from any of the other non-limiting embodiments.
- It should be appreciated that like reference numerals identify corresponding or similar elements throughout the several drawings. It should also be appreciated that although a particular component arrangement is disclosed in the illustrated embodiment, other arrangements will benefit herefrom.
- The foregoing description is exemplary rather than defined by the limitations within. Various non-limiting embodiments are disclosed herein, however, one of ordinary skill in the art would recognize that various modifications and variations in light of the above teachings will fall within the scope of the appended claims. It is therefore to be appreciated that within the scope of the appended claims, the disclosure may be practiced other than as specifically described. For that reason the appended claims should be studied to determine true scope and content.
Claims (10)
- A method for local repair to a damaged area of a multi-layer polyurethane erosion coating system on an airfoil surface of a fan blade, comprising:preparing the erosion coating adjacent to the damage by abrading and/or feathering; and cleaning the erosion coating adjacent to the damage;applying a paint primer onto a substrate in the damaged area; andapplying a filled epoxy paste to the paint primer in the damaged area.
- The method as recited in claim 1, wherein preparing the erosion coating system adjacent to the damaged area comprises abrading the erosion coating down to the substrate, wherein the substrate for the erosion coating system is an aluminum substrate.
- The method as recited in claim 1, wherein preparing the multi-layer polyurethane erosion coating system adjacent to the damaged area comprises feathering the erosion coating into the airfoil surface adjacent to the damaged area.
- The method as recited in claim 1, wherein the substrate for the erosion coating system is an aluminum substrate and the multi-layer polyurethane erosion coating on the substrate comprises a phosphoric acid anodize layer, a corrosion inhibiting epoxy bond primer, a corrosion inhibiting paint primer, and an elastomeric erosion coating as the outer layer.
- A component with a local repair to a multi-layer polyurethane erosion coating, comprising:
a local area of missing multi-layer polyurethane erosion coating, the local area filled with a filled epoxy paste over a substrate that forms an airfoil surface, and further comprising a paint primer between the filled epoxy paste and the substrate. - The component as recited in claim 5, wherein the substrate for the erosion coating system is an aluminum substrate and the multi-layer polyurethane erosion coating comprises a phosphoric acid anodize layer, a corrosion inhibiting epoxy bond primer, a corrosion inhibiting paint primer, and an elastomeric erosion coating, the elastomeric erosion coating as the outer layer.
- The component as recited in any one of claims 5-6 wherein said component is a gas turbine engine component.
- The component as recited in claim 7 wherein said component is a part in the airstream of the engine.
- The component as recited in any one of claims 5 to 8 wherein said component is an airfoil.
- The component as recited in any one of claims 5 to 9 wherein said component is a guide vane or a fan blade.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201562387453P | 2015-12-24 | 2015-12-24 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP3184180A1 EP3184180A1 (en) | 2017-06-28 |
EP3184180B1 true EP3184180B1 (en) | 2020-06-10 |
Family
ID=57681297
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP16204712.0A Active EP3184180B1 (en) | 2015-12-24 | 2016-12-16 | Local repair or remanufacture of polymeric erosion coatings |
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Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11260421B2 (en) | 2017-07-21 | 2022-03-01 | Raytheon Technologies Corporation | Method to strip and recoat erosion coatings applied to fan blades and structural guide vanes |
US20190024256A1 (en) * | 2017-07-21 | 2019-01-24 | United Technologies Corporation | Method to strip and recoat erosion coatings applied to fan blades and structural guide vanes |
US10677068B2 (en) * | 2018-01-18 | 2020-06-09 | Raytheon Technologies Corporation | Fan blade with filled pocket |
US10828667B1 (en) * | 2019-06-07 | 2020-11-10 | United Technologies Corporation | Removal of epoxies from metal substrates |
US11274950B2 (en) | 2019-06-17 | 2022-03-15 | United Technologies Corporation | Fabrication of high density sensor array |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6171704B1 (en) * | 1995-12-29 | 2001-01-09 | Sermatech International, Inc. | Coating for aerospace aluminum parts |
US7033673B2 (en) * | 2003-07-25 | 2006-04-25 | Analytical Services & Materials, Inc. | Erosion-resistant silicone coatings for protection of fluid-handling parts |
ES2860724T3 (en) * | 2004-05-24 | 2021-10-05 | Hontek Corp | Abrasion resistant coatings |
-
2016
- 2016-12-16 EP EP16204712.0A patent/EP3184180B1/en active Active
Non-Patent Citations (1)
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EP3184180A1 (en) | 2017-06-28 |
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