Abstract:
An apparatus for applying segmented ceramic coatings includes means for supporting and moving one or more substrates; one or more heat sources disposed proximate to one or more substrates, wherein at least one of the heat sources is positioned to apply a heat stream to pre-heat a thermal gradient zone on a surface of a substrate; a material deposition device disposed proximate to one or more heat sources, wherein the material deposition device is positioned to deposit a material on a deposition area located behind the thermal gradient zone on the surface; and means for monitoring a surface temperature of one or more substrates.
Abstract:
CERAMIC COATING SYSTEMS AND METHODSAn article has a metallic substrate. The substrate has a first surface region and a plurality of blind recesses along the first surface region. The substrate has perimeter lips at the openings of the plurality of recesses and extending partially over the respective associated recesses. A ceramic coating is along the first surface region.Figure 1.
Abstract:
THERMAL BARRIER COATING A bond coat is applied to a substrate of a gas turbine engine component the component. A barrier coat is applied atop the bond coat. The applying of the bond coat includes: applying a first layer having an as-applied first roughness; and applying a second layer atop the first layer, the second layer having an as- applied second roughness, greater than the first roughness. In the resulting coating system, the first and second layers may have different properties (e.g., greater porosity, pore size, and/or splat size for the second layer).
Abstract:
A powder port blow-off system for a plasma spray process includes a faceplate that includes a bore therein that is co-radially aligned with a nozzle of a plasma spray gun, which emits a plasma plume. A plurality of powder feed ports are arranged circumferentially around the nozzle for injecting a flow of powder particles toward the plasma plume. A plurality of powder port blow-offs are arranged circumferentially around the nozzle in order to direct blow-off gas across the powder feed ports. The powder port blow-offs are directed across the plasma plume to create a vortex for carrying away powder particles unconsumed by the plasma plume.
Abstract:
A turbine article includes a substrate with a geometric surface feature having a plurality of recesses recessed into the substrate. A ceramic topcoat is disposed over the geometric surface feature. The topcoat includes portions that are separated by faults extending through the topcoat from the geometric surface feature so the topcoat is segmented. A ceramic interlayer is disposed between the topcoat and the geometric surface feature.
Abstract:
A seal comprises a housing. A coating has at least two layers with a bond layer to be positioned between a housing and a second hard layer. The second hard layer is formed to be harder than the bond layer. The bond layer has a bond strength greater than or equal to 200 psi and less than or equal to 2000 psi. A gas turbine engine, and a method of forming a coating layer are also disclosed.
Abstract:
A method for protecting porous aluminum coatings includes the steps of: providing an orsomil suspension; and rating the porous aluminum coating with said orsomil suspension. The porous aluminum coating may be thermally sprayed coating.
Abstract:
One aspect of the disclosure involves a nib material comprising a polymeric matrix and carbon nanotubes in the matrix. In one or more embodiments of any of the foregoing embodiments, the matrix comprises a silicone. In one or more embodiments of any of the foregoing embodiments, the rub material is at least 1.0 mm thick. In one or more embodiments of any of the foregoing embodiments, the silicone is selected from the group consisting of dimethyl- and fluoro-silicone rubbers and their copolymers. In one or more embodiments of any of the foregoing embodiments, the carbon nanotubes at least locally have a concentration of 1-20% by weight.
Abstract:
A method comprises: thermal spray (416) of a first ceramic layer; sol infiltration (420) of ceramic particles into the first ceramic layer; and after the sol infiltration, thermal spray (434) of a second ceramic layer atop the first ceramic layer.