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Yamashita; Daiya
Saitama, JP
No. of patents:

Patent Number Title Of Patent Date Issued
6786452 Wing structure of airplane September 7, 2004
In a wing of an airplane, a front spar having a C-shape in section includes a web, flanges, and a reinforcing partition wall. An intermediate spar having an I-shape in section includes a web, flanges, and a reinforcing partition wall. Ribs can be positioned in a span direction by couplin
5807454 Method of maufacturing a leading edge structure for aircraft September 15, 1998
A leading edge structure for an aircraft has an outer wall, an inner wall disposed within the outer wall and including a partition with, the outer wall, the inner wall and the partition jointly defining a hot-air chamber, and a plurality of flow-rectifying fins or disposed in the hot-air

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