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 代理人
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