Structural component and fuselage of an aircraft or spacecraft
AssigneeAirbus Operations GmbH
InventorsHinnik Gensch, Thorsten Roming
Life of this patent
Estimating the term…
Abstract
A supporting component is provided for reinforcing the skin of an aircraft or spacecraft, for example a stringer or former, this component being configured as a closed profile (hollow profile), such that a system medium (M) can be conducted through the structural component. In this respect, the hollow profile itself serves as a load-bearing component.
Claims11
A structural component which is a load-receiving former for reinforcing a skin of an aircraft or spacecraft, the structural component comprising a closed hollow profile for receiving at least one system medium such that the system medium can be introduced into the hollow profile in a first location and removed from the hollow profile in a second location which is at a distance from the first location, wherein the structural component has a receiving stand by which the structural component can be attached to the skin, the receiving stand has a foot portion which can be positioned on the skin and can be attached to the skin, and a receiving portion which is configured for receiving the hollow profile.
Dependencies are inferred from the claim text.