Patent ID: 9482113
Filing Date: 2016-11-01
CPC Classification: B64C,B64D,F01D,F02C,Y02T

Claim Text:
1. An assembly for a propulsion system including a jet engine housed within a nacelle, the assembly comprising: a thermal blanket configured to at least partially surround the engine, and thermally shield at least a portion of the nacelle from heat energy radiated by the engine; a bracket orientation clip including a base and a plurality of anti-rotation tabs; a bracket for a fire detection system; and a fastening mechanism configured to connect the bracket to the nacelle; wherein the base is bonded to the blanket, and the tabs extend out from the base and away from the blanket; wherein the bracket orientation clip is arranged between the blanket and the bracket, and configured to limit or substantially prevent rotation of the bracket relative to the blanket; and wherein the fastening mechanism projects through the bracket, the bracket orientation clip and the thermal blanket.