PRE-COATING BURNISHING OF EROSION COATED PARTS

    公开(公告)号:SG139615A1

    公开(公告)日:2008-02-29

    申请号:SG2007025562

    申请日:2007-04-05

    Abstract: PRE-COATING BURNISHING OF EROSION COATED PARTS A gas turbine engine blade has a platform. A root depends from the platform and an airfoil extends from the platform. The airfoil has leading and trailing edges and pressure and suction sides. The blade has a substrate having a surface. A compressive stress exists below a first region of the surface. The first region extends over a majority of a streamwise perimeter of the airfoil at a location at a spanwise distance from the tip or more than 50% of a tip-to-platform span. A coating is on the surface including at the location.

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