Device for spacing electrical harnesses in a turbomachine
AssigneeSnecma
InventorsChristian Henry Mazelle, Guillaume Marcillaud
Life of this patent
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Abstract
A spacer device for spacing electrical harnesses in a turbomachine such as an airplane turboprop or turbojet is disclosed. The spacer device includes clips fastened on a support. A first clip is mounted on a harness via a retention device which prevents the spacer device from moving relative to the harness, and the spacer device includes a strip mounted around the first clip in order to close the first clip after a harness has been mounted in the first clip. The strip is fastened to the support in a non-releasable manner.
Claims10
A spacer device for spacing electrical harnesses in a turbomachine, the device comprising:
- clamping spring clips for clamping onto the harnesses, said clips being mounted spaced apart from one another on a common support,
- wherein a first clip is mounted on a first harness via retention means for preventing any translation of the device with respect to the first harness, and
- wherein the device includes a strip mounted around the first clip to close the first clip once the first harness has been mounted in the first clip, the strip being fastened in a non-releasable manner on said support.
Dependencies are inferred from the claim text.