Patent ID: 9316174
Filing Date: 2016-04-19
CPC Classification: F02K,F05D,Y10T

Claim Text:
1. A liner assembly for a gas turbine engine comprising: a liner defining an inner surface exposed to exhaust gases from the gas turbine engine; a duct spaced radially outward of the liner; and a hanger assembly supporting the liner relative to the duct, the hanger assembly including a body segment attached to the liner, a first washer disposed within an opening of the body segment, and a second washer disposed within the opening of the body segment, a portion of the first washer in abutting contact with a portion of the second washer within the opening of the body segment, the first washer and the second washer defining a gap therebetween, wherein the gap between the first washer and the second washer receives a portion of the body segment such that the body segment is movable relative to the first washer and the second washer, and an attachment member is seated on the first washer and the second washer and attached to the duct.