发明名称 AIRCRAFT WING FAN-TYPE FLAP DRIVE
摘要 FIELD: aircraft engineering.SUBSTANCE: flap dive comprises flaps, carriages, links, levers and translating drives. This device comprises flap turn-and-deflect kinematic systems. Turn system allows flap turn with angular shift relative to aircraft Z axis. Note here that as-extended flap stays at position whereat wing trailing edge is parallel with flap leading edge to make the clearance, invariable over the wing span. Deflect system deflects the flaps through preset angle. Note here that as-developed flap can turn about axis Z in flap weight beam. All displacement of the flap are actuated by the rotation of shaft-hole pair.EFFECT: higher efficiency of takeoff-landing performances, decreased weight and sizes.5 dwg
申请公布号 RU2539018(C1) 申请公布日期 2015.01.10
申请号 RU20140104270 申请日期 2014.02.06
申请人 FEDERAL'NOE GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "SIBIRSKIJ NAUCHNO-ISSLEDOVATEL'SKIJ INSTITUT AVIATSII IM. S.A. CHAPLYGINA" 发明人 SABEL'NIKOV VIKTOR IVANOVICH;KOLEVATOV JURIJ VITAL'EVICH;JAKOVLEV VLADIMIR VASIL'EVICH;TRUNOV VJACHESLAV ALEKSANDROVICH
分类号 B64C3/50 主分类号 B64C3/50
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