Removal of epoxies from metal substrates
A method of repairing a defectively manufactured multi-layer component having a substrate material and a primer layer includes applying, to the primer layer, a solvent that causes the primer layer to swell to form a swelled primer layer. The method also includes abrading away the swelled primer layer from the multi-layer component and rebuilding the multi-layer component by forming a new primer layer on the substrate material.
1. A method of repairing a defectively manufactured multi-layer component that includes a substrate material, a coating, a structural adhesive, and a primer layer, the method comprising:
removing the coating from the multi-layer component, wherein the coating is formed of a metal or alloy;
removing the structural adhesive from the multi-layer component and exposing the primer layer;
applying, to the primer layer, a solvent that causes the primer layer to swell to form a swelled primer layer;
abrading away the swelled primer layer from the multi-layer component;
rebuilding the multi-layer component by forming a new primer layer on the substrate material; and
rebuilding the multi-layer component by forming a new structural adhesive on the new primer layer, and a new coating on the new structural adhesive.
2. The method of claim 1 , wherein the multi-layer component also includes an anodized layer, the method further comprising:
chemically etching away the anodized layer from the multi-layer component; and
applying a new anodized layer to the multi-layer component, wherein the step of forming the new primer layer further comprising forming the new primer layer over the new anodized layer.
3. The method of claim 2 , wherein the substrate material is formed of aluminum.
4. The method of claim 1 , wherein the coating includes at least one of a sheath, an airfoil cover, a wear pad, or a seal.
5. The method of claim 1 , wherein the substrate material is formed of aluminum.
6. The method of claim 1 , wherein the primer layer and the new primer layer are toughened epoxies.
7. A method of repairing a damaged multi-layer component that includes a material substrate, an anodized layer, a primer layer, a structural adhesive, and a coating, the method comprising:
removing the coating from the multi-layer component, wherein the coating is formed of a metal or alloy;
removing the structural adhesive from the multi-layer component and exposing the primer layer;
applying, to the exposed primer layer, a solvent that swells the exposed primer layer to form a swelled primer layer;
abrading away the swelled primer layer from the multi-layer component;
chemically etching away the anodized layer from the multi-layer component;
forming a new anodized layer on the material substrate;
applying a new primer layer over the new anodized layer;
applying a new structural adhesive over the new primer layer; and
applying a new coating over the new structural adhesive.
8. The method of claim 7 , wherein the substrate material is formed of aluminum.
9. The method of claim 7 , wherein the primer layer and the new primer layer are toughened epoxies.