Abstract: A method for patching a damaged polymeric erosion coating (250) on a gas turbine engine component. The method comprises removing a portion of the coating around a damage site (200; 202; 204) and applying a pre-formed coating patch (220).

Abstract: A method for patching a damaged polymeric erosion coating (250) on a gas turbine engine component. The method comprises removing a portion of the coating around a damage site (200; 202; 204) and applying a pre-formed coating patch (220).

Abstract: A silicone rubber coating material to be bonded to substrates such as on gas turbine components is made by providing a silicone rubber layer having a fiber layer attached to one side of the silicone rubber layer prior to its molding into a compound. The fibers may be either woven fabrics or random fiber sheets and the fiber layer may be from about 3 mils to about 30 mils (0.0762 mm to 0.762 mm) thick.

Abstract: A method includes positioning a layer of adhesive between a first structural component and a second structural component, positioning a first evaluation film between the first structural component and the layer of adhesive, curing the adhesive at least partially, separating the first structural component and the first evaluation film by a relative movement therebetween, and inspecting bond line quality of the adhesive.

Abstract: A mandrel comprising a rigid inner core and an elastomeric outer layer that at least partially surrounds the rigid inner core, wherein the elastomeric outer layer is adapted to expand during a molding process to seal a cavity to prevent incursion of material injected during the molding process.

Abstract: A process for manufacturing a composite structure includes the steps of disposing a removable adhesive material in contact with a first surface of a reusable composite structure; disposing a first surface of an expendable composite structure in contact with the removable adhesive material to form a composite structure assembly; and curing the composite structure assembly.

Abstract: The present invention relates to a pressure application device for curing an adhesive on a component, particularly components of complex geometries. The device comprises a pair of jaws, at least one spring recessed into a cavity defined within the first jaw, and a cap. A first end of a spring partially extends into the cavity and a second end of the spring contacts the cap. When force is applied to the cap, the cap transmits the force through the spring to the first jaw. In order to limit the separation of the cap from the first jaw, a retainer is used.

Abstract: A mandrel comprising a rigid inner core and an elastomeric outer layer that at least partially surrounds the rigid inner core, wherein the elastomeric outer layer is adapted to expand during a molding process to seal a cavity to prevent incursion of material injected during the molding process.