CPC B64C 3/26 (2013.01) [B64C 3/20 (2013.01); B64C 3/24 (2013.01)] | 20 Claims |
1. An aircraft component comprising:
a structural foam having a predetermined shape;
an outer flange located near a first end of the structural foam;
an inner flange located near a second end of the structural foam;
a web skin encapsulating the inner flange and at least a portion of the structural foam, wherein the structural foam is affixed to the web skin, and wherein the aircraft component comprises a portion of a blended wing body aircraft (BWB), the BWB having no demarcation between a wing and a main body of the BWB.
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