Patent ID: 9140287
Filing Date: 2015-09-22
Classification: B64D,F16B,Y10T

Abstract:
1. A fastener assembly for mounting a component to a bracket attached to an inner surface of a skin of an aircraft wing such that the component is thermally and electrically isolated from the bracket, the component and bracket each having mounting holes, wherein the fastener assembly comprises a fastening element having a shaft to extend through said holes, first and second isolating members mountable on the shaft on either side of the bracket such that the bracket is sandwiched between said first and second isolating members and, a retaining element threadingly engageable with the shaft protruding through the second isolating member to clamp said first and second isolating members together against said bracket, wherein one of said isolating members has a central portion that protrudes through said mounting hole in the bracket and the other isolating member comprises a recess to receive said central portion.