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US 2011/0031350 A1Published application
Componet, in particular a shell component, which can be joined thermally and/or mechanically, for building a fuselage section of an aircraft
AssigneeAirbus Operations GmbH
InventorsCihangir SAYILGAN, Robert Alexander GOEHLICH
Life of this patent
Estimating the term…
Abstract
A component for building a fuselage section of an aircraft includes a border area connectable to a corresponding further border area of a further component so as to form an electrically conductive joint, wherein the component includes a composite structure
Claims15
A component for building a fuselage section of an aircraft comprising:
- a border area connectable to a corresponding further border area of a further component so as to form an electrically conductive joint, wherein the component includes a composite structure.
A fuselage section of an aircraft comprising:
- a first component including a first composite material having a first border area;
- and
- a second component including a second composite material having a second border area connected to the first border area so as to form an electrically conductive joint.
Dependencies are inferred from the claim text.