发明名称 |
Tailless aircraft, has no elevator or rudder and thrust path is adjustable relative to fuselage |
摘要 |
<p>An aircraft with fuselage (2) and at least one main wing for generating drive (lift) and at least one motor for generating thrust, in which the motor (6) is not arranged on the wing (2). No elevator or rudder is provided and the thrust path can be adjusted relative to the fuselage for controlling the aircraft (1).</p> |
申请公布号 |
DE10322412(A1) |
申请公布日期 |
2004.12.02 |
申请号 |
DE2003122412 |
申请日期 |
2003.05.16 |
申请人 |
SCHREIBER, PAUL |
发明人 |
SCHREIBER, PAUL |
分类号 |
B64C15/12;B64C39/02;B64C39/10;(IPC1-7):B64C15/12 |
主分类号 |
B64C15/12 |
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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