发明名称 DEVICE TO CONTROL AIRCRAFT WING FLAP SYNCHRONISM
摘要 FIELD: transport.SUBSTANCE: invention relates to aircraft engineering. Proposed device comprises control cable connected with flaps to move jointly therewith. Control cable lay-out path extends from the first point to second point, located, either one or both, on stationary elements of aircraft wing structure.EFFECT: simplified design.15 cl, 6 dwg
申请公布号 RU2475423(C2) 申请公布日期 2013.02.20
申请号 RU20080115258 申请日期 2008.04.17
申请人 LIBKHERR-AEHROSPEJS LINDENBERG GMBKH 发明人 SHIFEL'BUSH BERND
分类号 B64D45/00;G08B23/00 主分类号 B64D45/00
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