发明名称 AIRCRAFT UNDERCARRIAGE SECTION FLAP CONTROL DEVICE
摘要 FIELD: transport.SUBSTANCE: invention relates to aircraft engineering. Control device comprises permanent mechanical joint coupled with flap and undercarriage to convert displacement of the latter between retracted position and extended position or to its reciprocation. This causes opening and closing of flaps in displacement of undercarriage between said positions. Said permanent joint comprises drive lever articulated with undercarriage element and coupled with sole link with aircraft fixed point to allow reciprocation relative to undercarriage element.EFFECT: simplified control device and section design.2 cl, 4 dwg
申请公布号 RU2527604(C2) 申请公布日期 2014.09.10
申请号 RU20120103558 申请日期 2010.07.05
申请人 MESS'E-BJUGATTI-DOVTI 发明人 ALONZO KRIST'JAN;BRIJAN KRIS;LONEH ARNO;RUSHUZ FREDERIK
分类号 B64C25/16 主分类号 B64C25/16
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