Abstract: An air seal for use in a gas turbine engine is disclosed. The seal includes a seal substrate, and an abradable layer on the substrate, with the abradable including a thermoset polymer and a thermoplastic polymer. The abradable may also include a filler to add porosity, or provide lubrication, to enhance abradability.
Type:
Grant
Filed:
December 17, 1999
Date of Patent:
March 5, 2002
Assignee:
United Technologies Corporation
Inventors:
William John Dalzell, Jr., Stuart Alan Sanders, George Lee Crawford, Frederick Clell Walden, William J. Woodard