Back to results
US 9,168,997 B2Granted
Aircraft conduit harness retention system
AssigneeAirbus Operations GmbH
InventorsJack Blanchard, David Routledge
Life of this patent
Estimating the term…
Abstract
A conduit harness retention system has a base, a first spacer, a second spacer and a cap which snap-fit together to retain P-clip harnesses in position spaced from an aircraft fuselage.
Claims11
An aircraft conduit harness retention system comprising:
- a base having a flange attachment formation for attachment to an aircraft component at a first end and a first mating formation at a second end;
- a spacer having a second mating formation at a first end and a mating formation identical to the base first mating formation and a second end;
- a cap having a mating formation identical to the spacer first end;
- and
- a conduit harness separate from the base and the spacer, wherein said conduit harness includes a wire loom receiving portion and a flange connected to the wire loom receiving formation, the flange having a bore defined therethrough,
- wherein the bore of the flange is engaged by at least one of the first mating formation and second mating formation and the first mating formation and the second mating formation are engaged via a snap-fit to clamp the flange of the conduit harness between the base and spacer or cap such that the conduit harness is offset from the aircraft component.
3 more elements
An aircraft conduit harness retention system comprising:
- a base having a flange attachment formation for attachment to an aircraft component at a first end and a first mating formation at a second end;
- at least one spacer having a second mating formation at a first end and a mating formation identical to the base first mating formation and a second end;
- a cap having a mating formation identical to the spacer first end;
- and
- at least one conduit harness separate from the base and the spacer, wherein said conduit harness includes a wire loom receiving portion and a flange connected to the wire loom receiving formation, the flange having a bore defined therethrough,
- wherein the bore of the flange is engaged by at least one of the first mating formation and second mating formation and the first mating formation and the second mating formation are engaged via a snap-fit to clamp the flange of the conduit harness between the base and spacer or cap such that the conduit harness is offset from the aircraft component.
3 more elements
Dependencies are inferred from the claim text.