Structural component with rib and cross member element
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United States of America Patent
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May 14, 2013
Issued Date -
N/A
app pub date -
Dec 15, 2009
filing date -
Jun 29, 2007
priority date (Note) -
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Abstract
The present invention provides a fuselage structure for an aircraft or spacecraft with an outer skin. The fuselage structure comprises a rib element for stiffening the outer skin and ad cross member element. Here the rib element is bent in the shape of an arc to correspond to an inner contour of the outer skin. The cross member element connects two arc sections of the rib element transversely to each other. The cross member element has a higher strength than the rib element. From another point of view the invention provides an aircraft with such a fuselage structure.
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