Structural component particularly for an aircraft

Details Structural component particularly for an aircraft Structural component particularly for an aircraft

F - Mech Eng,Light,Heat,Weapons

16

S

F16S 1/10 (2006.01) B64C 1/12 (2006.01)

Patent

CA 2328653

A structural component for example an aircraft door or aircraft body section is cast of lightweight metals as an integral structure with an outer skin reinforced by stiffening ribs forming a first grid structure and by stiffening walls forming a second gird structure integrally connected to the first grid structure as a result of casting. The side opposite the skin on the second grid structure is preferably covered by a further inner skin, for example secured by casting or by an adhesive.

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