Abstract: A component suitable for use in a gas turbine engine. The component includes a substrate defining a surface of the component and has a first surface and a second surface. At least one aperture extends through the substrate from the first surface to the second surface, and has a first open area. The component has a first coating on at least one of the first surface and the second surface adjacent to the at least one aperture. The component also has a second coating overlying the first coating adjacent to the at least one aperture, such that at least a portion of the first coating is exposed adjacent to the at least one aperture. The first coating defines a second open area which is smaller than the first open area.

Abstract: A method for applying a plasma prayed coating using liquid injection is disclosed. The method includes providing a mixture of a liquid and solid particles. The solid particles are constituents of a thermal barrier coating. The mixture is injected into a plasma jet of a plasma spray device and the plasma jet is directed toward a substrate to deposit a gradient film formed from the constituents onto the substrate.

Abstract: A protected article includes a substrate having a surface, and a protective system overlying and contacting a first portion of the surface of the substrate. The protective system has a nickel-base superalloy bond coat, an aluminide layer overlying and contacting the bond coat, and a dense vertically microcracked ceramic thermal barrier coating overlying and contacting the aluminide layer.

Abstract: A method for adjusting the airflow in a turbine component having a plurality of airflow holes. The method comprises the step of depositing an overlay metallic coating on the surface of the turbine component in a manner such that at least some of the airflow holes are partially filled such that the volume of the partially filled airflow holes is changed so as to adjust the airflow through the turbine component. Also provided is a turbine component having a plurality of airflow holes, at least some of the airflow holes being partially filled with the overlay metallic coating to change the volume thereof so as to adjust the airflow through the turbine component.

Abstract: A method applying a thermal barrier coating to a metal substrate, or for repairing a thermal barrier coating previously applied by physical vapor deposition to an underlying aluminide diffusion coating that overlays the metal substrate. The aluminide diffusion coating is treated to make it more receptive to adherence of a plasma spray-applied overlay alloy bond coat layer. An overlay alloy bond coat material is then plasma sprayed on the treated aluminide diffusion coating to form an overlay alloy bond coat layer. A ceramic thermal barrier coating material is plasma sprayed on the overlay alloy bond coat layer to form the thermal barrier coating. In the repair embodiment of this method, the physical vapor deposition-applied thermal barrier coating is initially removed from the underlying aluminide diffusion coating.

Abstract: A plumbing device includes a radially outwardly and resiliently expansible sealing plug carried on the front end of an elongated axial shaft. An elongated cylinder disposed about the shaft transmits axial movement to the plug from a jack mechanism near the rear end of the shaft so as to cause expansion of the plug into sealing engagement with the inner surface of a pipe in which it is positioned. An external shackle is clamped about the pipe and carries a pair of elongated threaded rods which extend rearwardly beyond the jack mechanism so that a rear lock gate plate can be placed over the axial shaft and secured on each of the threaded rods so as to abut the jack mechanism and so prevent rearward axial displacement of the plug within the pipe under the action of fluid pressure therein.