发明名称 CONTROL METHOD FOR AIRCRAFT (AC) OF HELICOPTER TYPE
摘要 FIELD: transport.SUBSTANCE: invention relates to aircraft engineering, particularly, to control methods for helicopter-type ACs. AC control method includes AC centre-of-gravity shift relative to propulsive thrust, where this shift is performed over spherical surface with its centre located outside AC, or cylindrical surface with its centreline located outside AC. Radius of spherical or cylindrical surface can be indefinitely great. Herewith, propulsor shifting can be translational.EFFECT: invention reduces dimensions of helicopter-type aircraft control system.3 cl, 2 dwg
申请公布号 RU2534159(C2) 申请公布日期 2014.11.27
申请号 RU20130105961 申请日期 2013.02.12
申请人 LENTOV IGOR' VIKTOROVICH 发明人 LAPSHIN SERGEJ ALEKSANDROVICH;LENTOV IGOR' VIKTOROVICH;MJAKISHEV SERGEJ VLADIMIROVICH;KHARITONOV TIMUR ZAUROVICH
分类号 B64C27/04;B64C29/00 主分类号 B64C27/04
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