Patent ID: 9212764
Filing Date: 2015-12-15
Classification: F16L,H02G

Abstract:
1. An attachment device for attaching an electrical harness on a structure of an aircraft, the attachment device comprising: a support connected to the structure; a body with at least two jaws, at least one of the jaws being movable along a reference plane perpendicular to a path direction between a first open position in which the at least two jaws enable an insertion of at least one harness and a second closed position in which the at least two jaws keep an at least one harness in a position; and a retainer strip in a form of a blade comprising free ends that are attachably inserted within the support allowing for the at least two jaws to be maintained in the second closed position and the body to be flattened against the support; wherein the at least one harness follows the path direction; and wherein the body comprises three jaws, a first jaw which cooperates with the at least two jaws, each connected to the first jaw via an articulation zone, the articulation zones being spaced apart as far as possible so that openings of the at least two jaws are oriented toward one another.