METHOD TO STRIP AND RECOAT EROSION COATINGS APPLIED TO FAN BLADES AND STRUCTURAL GUIDE VANES

    公开(公告)号:US20190022698A1

    公开(公告)日:2019-01-24

    申请号:US15656275

    申请日:2017-07-21

    Abstract: A method of repairing an erosion coating coupled to a substrate, wherein the coating comprises an anodization layer on the substrate, a bond primer layer on the anodization layer, a corrosion-resistant primer on the bond primer, and an erosion coating on the corrosion-resistant primer. The method comprises abrading an erosion coating; abrading a corrosion-resistant primer; creating an abraded surface comprising a bond primer over an anodization layer coupled to the substrate, applying a sol-gel adhesion promoter layer to said abraded surface; applying a corrosion-resistant layer over the sol-gel adhesion promoter layer; and applying an erosion coating layer over the corrosion-resistant layer.

    GAS TURBINE ENGINE NOSE CONE ASSEMBLY
    8.
    发明申请

    公开(公告)号:US20200010172A1

    公开(公告)日:2020-01-09

    申请号:US16504043

    申请日:2019-07-05

    Abstract: A nosecone assembly having an axially extending centerline is provided. The assembly includes a nosecone body and at least one access panel. The nosecone body has at least one wall that defines an interior cavity. The wall has an interior surface contiguous with the interior cavity, and at least one window aperture extending through the wall. The access panel has first and second face surfaces. The access panel is attached to the wall interior surface within an attachment region that includes first and second attachment region portions partially contiguous with one another. The first and second attachment region portions define an interior unattached region, and the interior unattached region is aligned with the window aperture.

    METHOD TO STRIP AND RECOAT EROSION COATINGS APPLIED TO FAN BLADES AND STRUCTURAL GUIDE VANES

    公开(公告)号:US20190024256A1

    公开(公告)日:2019-01-24

    申请号:US15656262

    申请日:2017-07-21

    Abstract: A method of repairing an erosion coating coupled to a substrate, wherein the coating comprises an anodization layer on the substrate, a bond primer layer on the anodization layer, a corrosion-resistant primer on the bond primer, and an erosion coating on the corrosion-resistant primer the method comprising abrading an erosion coating; abrading a corrosion-resistant primer; creating an abraded surface comprising a bond primer over an anodization layer coupled to the substrate, chemically etching the anodization layer; abrading the bond primer; applying an anodization layer to the substrate; applying a bond primer layer over the anodization layer; applying a corrosion-resistant layer over the bond primer layer; and applying an erosion coating layer over the corrosion-resistant layer.

    Gas turbine engine nose cone assembly

    公开(公告)号:US11097831B2

    公开(公告)日:2021-08-24

    申请号:US16504043

    申请日:2019-07-05

    Abstract: A nosecone assembly having an axially extending centerline is provided. The assembly includes a nosecone body and at least one access panel. The nosecone body has at least one wall that defines an interior cavity. The wall has an interior surface contiguous with the interior cavity, and at least one window aperture extending through the wall. The access panel has first and second face surfaces. The access panel is attached to the wall interior surface within an attachment region that includes first and second attachment region portions partially contiguous with one another. The first and second attachment region portions define an interior unattached region, and the interior unattached region is aligned with the window aperture.

Patent Agency Ranking