Patent ID: 7581700
Filing Date: 2009-09-01
Classification: B64D,F16L,Y10T

Abstract:
1. An aircraft system, comprising: a fluid conduit carried by an aircraft; a first housing fixedly attached to the fluid conduit, the first housing including a first attachment feature having a projection extending outwardly from the housing; a second housing fixedly attached to the fluid conduit and spaced apart from the first housing, the second housing including another first attachment feature; a support member having a first attachment portion positioned proximate to the first housing and a second attachment portion proximate to the second housing, the first attachment portion including a first support member aperture positioned over at least a portion of the first attachment feature and the second attachment portion including a second support member aperture positioned over at least a portion of the other first attachment feature; and a first adjustable fitting coupling the first attachment portion of the support member to the first housing, and a second adjustable fitting coupling the second attachment portion of the support member to the second housing, each adjustable fitting including