Method for carrying out method for implementing energy conversion installation service measures, and energy conversion installation
US-2024392684-A1 · Nov 28, 2024 · US
US2016369635A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016369635-A1 |
| Application number | US-201414903872-A |
| Country | US |
| Kind code | A1 |
| Filing date | Jul 9, 2014 |
| Priority date | Jul 9, 2013 |
| Publication date | Dec 22, 2016 |
| Grant date | — |
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A composite component is disclosed. The composite component may comprise a metal plating deposited on a surface of the composite component, and a metallic feature adhesively bonded to the metal plating. The composite component may further comprise an adhesive layer between the metal plating and the metallic feature. The metal plating may provide a metal-to-metal interface between the surface of the composite component and the metallic feature.
Opening claim text (preview).
What is claimed is: 1 . A composite component, comprising: a metal plating deposited on a surface of the composite component; a metallic feature adhesively bonded to the metal plating; and an adhesive layer between the metal plating and the metallic feature. 2 . The component of claim 1 , wherein the metal plating provides a metal-to-metal interface between the surface of the composite component and the metallic feature. 3 . The component of claim 2 , wherein the composite component is formed from a polymeric matrix. 4 . The component of claim 3 , wherein the polymeric matrix is reinforced with fibers selected from the group consisting of metal fibers, carbon fibers, and glass fibers. 5 . The component of claim 3 , wherein the polymeric matrix is a thermoplastic material or a thermoset material. 6 . The component of claim 5 , wherein the metallic feature is formed from a metal or a metal alloy selected from the group consisting of titanium, nickel, and a nickel-cobalt alloy. 7 . The component of claim 5 , wherein the composite component is an airfoil of a gas turbine engine. 8 . The component of claim 7 , wherein the surface of the composite component is a leading edge of the airfoil, and wherein the metallic feature is a sheath configured to protect the leading edge. 9 . A method for fabricating a composite component adhesively bonded to a metallic feature, comprising: forming the composite component in a desired shape; depositing a metal plating on a surface of the composite component; selecting an adhesive for bonding the metallic feature to the metal plating of the composite component; and adhesively bonding the metallic feature to the metal plating using the selected adhesive. 10 . The method of claim 9 , wherein selecting the adhesive for bonding the metallic feature to the metal plating comprises selecting an adhesive capable of providing a bond at a metal-to-metal interface. 11 . The method of claim 10 , wherein forming the composite component in a desired shape comprises forming the composite component from a thermoplastic material or a thermoset material. 12 . The method of claim 10 , wherein forming the composite component in a desired shape comprises forming the composite component from a thermoplastic material or a thermoset material, the thermoplastic material or the thermoset material having fibers embedded therein. 13 . The method of claim 12 , wherein forming the composite component in a desired shape further comprises forming the composite component by a method selected from the group consisting of injection molding, compression molding, blow molding, additive manufacturing, and composite layup. 14 . The method of claim 13 , wherein depositing the metal plating on the surface of the composite component comprises: preparing the surface of the composite component to receive a catalyst by etching, abrasion, or reactive-ion etching; depositing a catalyst layer on the surface of the composite component; depositing a first layer on the catalyst layer by electroless deposition; depositing a second layer on the first layer by electrolytic deposition, the second layer being conductive; and depositing the metal plating on the second layer. 15 . The method of claim 14 , wherein depositing the metal plating on the second layer is performed by a method selected from the group consisting of electroplating, electroless plating, and electroforming. 16 . A composite component adhesively bonded to a metallic feature, the composite component being formed by a method comprising: forming the composite component in a desired shape; depositing a metal plating on a surface of the composite component; selecting an adhesive for bonding the metallic feature to the metal plating of the composite component; and adhesively bonding the metallic feature to the metal plating using the selected adhesive. 17 . The composite component of claim 16 , wherein selecting the adhesive for bonding the metallic feature to the metal plating comprises selecting an adhesive capable of providing a bond at a metal-to-metal interface. 18 . The composite component of claim 17 , wherein forming the composite component in a desired shape comprises forming the composite component from a thermoplastic material or a thermoset material. 19 . The composite component of claim 19 , wherein depositing the metal plating on the surface of the composite component comprises: preparing the surface of the composite component to receive a catalyst by etching, abrasion, or reactive-ion etching; depositing a catalyst layer on the surface of the composite component; depositing a first layer on the catalyst layer by electroless deposition; depositing a second layer on the first layer by electrolytic deposition, the second layer being conductive; and depositing the metal plating on the second layer. 20 . The composite component of claim 19 , wherein the composite component is an airfoil of a gas turbine engine, and wherein the metallic feature is a sheath configured to protect a leading edge of the airfoil.
Fibrous particles · CPC title
Two or more layers only obtained by electroless plating · CPC title
Two or more layers with at least one layer obtained by electroless plating and one layer obtained by electroplating · CPC title
Metals, alloys or intermetallic compounds · CPC title
Inorganic materials other than provided for in groups F05D2300/10 - F05D2300/2291 · CPC title
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