发明名称 Aircraft with safety tail unit
摘要 Aircraft having supersonic and subsonic flight capabilities which utilize variable geometry tail units and fixed front planes to generally improve airworthiness and safety of aircraft during takeoff and landing, and which additionally have a reduced air resistance during high-speed flight and thus save propulsion energy.
申请公布号 US4008867(A) 申请公布日期 1977.02.22
申请号 US19750633994 申请日期 1975.12.15
申请人 KANIUT, HERBERT M. 发明人 KANIUT, HERBERT M.
分类号 B64C3/00;(IPC1-7):B64C5/02 主分类号 B64C3/00
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