发明名称 HIGH-CAPACITY AIRCRAFT
摘要 FIELD: transportation. ^ SUBSTANCE: high capacity aircraft includes a wing made in technique of "combined with fuselage wing" consisting of centre wing of increased thickness provided with departments for passengers or load accommodation front edges of which have high backward sweep, arrow-type outer wings, resting on fishtails contiguous with center wing. Lower surfaces of center wing, outer wings and fishtail form single lower surface of wing. Upper surface of center wing is turned up relative to surface of outer wings. Rudder unit is made as two keels. Upper surface of center wing is provided with longitudinal anti-stall fences, stretching from ahead of center wing to keels while being in one plane with them. Rear edge of center wing is made straight. Outer wings are made V-shaped with positive angle when seen from front. ^ EFFECT: improvement of aircraft take-off and landing characteristics. ^ 4 cl, 5 dwg
申请公布号 RU2335430(C1) 申请公布日期 2008.10.10
申请号 RU20070106515 申请日期 2007.02.21
申请人 ZAKRYTOE AKTSIONERNOE OBSHCHESTVO NAUCHNO-METODICHESKIJ TSENTR "NORMA" (ZAO NMTS "NORMA") 发明人 PODKOLZIN VASILIJ GRIGOR'EVICH;SHVEDOV VLADIMIR TARASOVICH;DMITRIEV VLADIMIR GRIGOR'EVICH;POLUNIN IGOR' MIKHAJLOVICH;ZINOV'EV DENIS MIKHAJLOVICH
分类号 B64C1/00 主分类号 B64C1/00
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