| 发明名称 |
DEVICE FOR ENHANCING LATERAL CONTROLLABILITY OF AIRCRAFT |
| 摘要 |
FIELD: aeronautical engineering. SUBSTANCE: device is made in form of flaperon with control surface mounted on it in accordance with wing span. Control surface deflects up and down relative to flap or flaperon. EFFECT: enhanced lateral controllability. 4 dwg |
| 申请公布号 |
RU94022712(A) |
申请公布日期 |
1996.08.27 |
| 申请号 |
RU19940022712 |
申请日期 |
1994.06.10 |
| 申请人 |
STAVROPOL'SKOE VYSSHEE AVIATSIONNOE INZHENERNOE UCHILISHCHE PVO IM.MARSHALA AVIATSII V.A.SUDTSA |
发明人 |
POPOV V.N.;USTINOV A.V. |
| 分类号 |
B64C9/04 |
主分类号 |
B64C9/04 |
| 代理机构 |
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代理人 |
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