发明名称 Travelling tail-unit with circular arc motion
摘要 Aircraft having subsonic and supersonic flight capabilities which utilize travelling tail units with circular arc motions, connected with the rear fuselage by means of two arm-frames that swing upward and rearward and vice versa, to generally increase stability and control of aircraft during low-speed flight and to reduce accidents at zero altitude operations.
申请公布号 US4037808(A) 申请公布日期 1977.07.26
申请号 US19760659140 申请日期 1976.02.18
申请人 KANIUT, HERBERT 发明人 KANIUT, HERBERT
分类号 B64C3/00;(IPC1-7):B64D33/02;B64C5/10 主分类号 B64C3/00
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