Patent ID: 9630722
Date: 2017-04-25
CPC Classifications: B64C,B64D,F16L

Claim:
1. A routing support for a line fastened in an opening in a structural component of an aircraft, the line comprised of two conduits connected end-to-end along a longitudinal axis, the routing support comprising: an outer body cooperating with a fastener configured to fasten the outer body in the aircraft structural component opening; a housing structure comprised of two accommodating parts for accommodating respective ends of the two conduits placed end-to-end; and a flexible interface resiliently connecting the housing structure to the outer body, wherein the flexible interface is integral and a single piece with the outer body and the housing structure, the flexible interface being attached to the two accommodating parts so as to physically distance them from the outer body and being comprised of a material having a bending capability so as to permit by bending limited translation and limited rotation of each of the two accommodating parts, and thus each of the two respective conduits with respect to the outer body, wherein the outer body and the housing structure are created by simultaneous or sequential bi-material injection with the flexible interface, and wherein the flexible interface is a different material from the material of the outer body and the housing structure.