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Inventor: Yamashita; Daiya
Address: Saitama, JP
No. of patents: 2
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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