Abstract: An abrasive coating for a substrate of a component in a gas path exposed to a maximum temperature of 500 degree Fahrenheit, comprising: a plurality of grit particles adapted to be placed on a top surface of the substrate; a matrix material bonded to the top surface; the matrix material partially surrounds the grit particles, wherein the grit particles extend above the matrix material relative to the top surface; and a film of oxidant resistant coating applied over the plurality of grit particles and the matrix material.
Type:
Grant
Filed:
July 19, 2018
Date of Patent:
June 8, 2021
Assignee:
Ratheon Technologies Corporation
Inventors:
Kevin Seymour, Christopher W. Strock, Thomas D. Kasprow
Abstract: A gas turbine engine component array includes first and second components each having a platform. The platforms are arranged adjacent to one another and provide a gap. A seal is arranged circumferentially between the first and second components and in engagement with the platforms to obstruct the gap. A cooling hole is provided in the seal and is in fluid communication with the gap. The cooling hole has an increasing taper toward the gap.
Abstract: A heat shield for a gas turbine engine includes a radial heat shield flange that extends in a circumferential direction and forms a ring. A plurality of bosses extend from a first axial side of the radial heat shield flange. There is a plurality of guide pins. One of the plurality of guide pins extends from a corresponding one of the plurality of bosses.
Type:
Grant
Filed:
April 30, 2018
Date of Patent:
September 15, 2020
Assignee:
RATHEON TECHNOLOGIES CORPORATION
Inventors:
Jonathan Jeffery Eastwood, Adam Lee Hart, Brian Craig, Luis Miguel Ayalde, Brian Levy