发明名称 |
DEPLOYABLE WING |
摘要 |
The deployable wing (1) of the present invention comprises an internal structure having diverging leading edge spars (7) attached to a keel spar (11) and cross spars (9) to form a delta wing configuration. This internal structure is enclosed within a volume defined by a fabric sail having an upper section (3a), a lower section (3b), and fabric ribs (5) disposed therebetween. This fabric sail volume is internally pressurized through a ram air intake (15) at the nose stagnation point. This deployable wing can be folded and deployed in the air.
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申请公布号 |
WO9514609(A1) |
申请公布日期 |
1995.06.01 |
申请号 |
WO1994US13032 |
申请日期 |
1994.11.14 |
申请人 |
USBI, CO. |
发明人 |
FISHER, JEFFREY, A.;MILLER, EDWARD, V.;VAN DAM, DENNIS |
分类号 |
B64C31/028;(IPC1-7):B64C31/028 |
主分类号 |
B64C31/028 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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