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US 9,040,821 B2Granted
Aircraft cable routing harness
AssigneeAirbus Operations GmbH
InventorsJack Blanchard, Anthony Bryant
Life of this patent
Estimating the term…
Abstract
A harness is provided comprising a body having a series of electrical conductors embedded therein and substantially running along the length thereof. The body may be part of a structural component such as stringer.
Claims19
An aircraft fuel tank assembly, comprising:
- an aircraft wing having an upper skin and a lower skin defining a fuel tank;
- and,
- a fuel quantity installation cable routing harness within the fuel tank, the fuel quantity installation cable routing harness comprising:
- an elongate body having an embedded conductor extending along its length;
- and,
- at least one connector extending from a base attached to one of upper or lower skins to the elongate body to provide an air gap between the elongate body and the base.
3 more elements
An aircraft fuel tank assembly, comprising:
- an aircraft wing having a wing skin defining a fuel tank;
- and,
- a fuel quantity installation cable routing harness within the fuel tank, the fuel quantity installation cable routing harness comprising:
- an elongate body having an embedded conductor extending along its length;
- at least one resilient arm extending from a base attached to the wing skin to the elongate body to provide an air gap between the elongate body and the base.
2 more elements
An aircraft fuel tank assembly, comprising:
- an aircraft wing having a wing skin defining a fuel tank;
- and,
- a fuel quantity installation cable routing harness within the fuel tank, the fuel quantity installation cable routing harness comprising:
- an elongate body having an embedded conductor extending along its length;
- a base attached to a lower surface of said wing skin, and a pair of resilient arms extending from said base to the elongate body to provide an air gap between the elongate body and the base.
2 more elements
Dependencies are inferred from the claim text.