发明名称 |
Aircraft configuration for micro and mini auv |
摘要 |
<p>An aircraft arrangement for Mini or Micro UAV comprising a fore wing (14) and an aft wing (12) in tandem closed-coupled arrangement. The aft wing (12) has side panels (18) and control surfaces (19), and tapered planform with positive sweep, while the fore wing (14) has non-positive trailing edge sweep. The fore wing (14) and the aft wing (12) are disposed at different height, and the aircraft arrangement has no other wings or tail arrangements.</p> |
申请公布号 |
IL174498(A) |
申请公布日期 |
2014.11.30 |
申请号 |
IL20060174498 |
申请日期 |
2006.03.23 |
申请人 |
ISRAEL AEROSPACE INDUSTRIES LTD.;MICHAEL SHEPSHELOVICH;MOSHE STEINBUCH;MARIO SLETEAN;DAVID ELI LEVY |
发明人 |
MICHAEL SHEPSHELOVICH;MOSHE STEINBUCH;MARIO SLETEAN;DAVID ELI LEVY |
分类号 |
B64C;B64C39/02;B64D15/16 |
主分类号 |
B64C |
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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