Patent ID: 8919134

Claim:
An assembly for a gas turbine engine, comprising: an outer radial housing having an outer surface; an inner radial housing disposed within the outer radial housing; and a linkage connected to the inner radial housing and the outer radial housing and removable from both the inner radial housing and the outer radial housing; a first bracket connected to the inner radial housing; a first leg and a second leg intersecting one another and connected to the first bracket, the first leg and the second leg are substantially aligned along a common plane; a second bracket extending from a distal portion of the first leg and a third bracket extending from a distal portion of the second leg, the second bracket and the third bracket orientated so as to extend in opposite directions from one another in substantially a same plane; a slot in the outer radial housing extending circumferentially around a portion of the outer radial housing, wherein the first leg and the second leg both extend through the slot, and wherein the second bracket and the third bracket interface with the outer surface of the outer radial housing, are connected thereto.