发明名称 LANDING FLAP DRIVE SYSTEM
摘要 FIELD: transport. ^ SUBSTANCE: invention relates to aircraft engineering, namely to landing flap drive system. Drive system is built in guide rail of landing flap and comprises first drive motor to displace landing flap, second drive motor and actuator to drive landing flap. Actuator drive mechanism is driven by first drive motor. Drive system comprises also locking device to lock landing flap and emergency unit to control first motor. First and second motors are timed by electronic means with mechanical linkage between said motors. ^ EFFECT: perfected landing flap drive system. ^ 8 cl, 9 dwg
申请公布号 RU2399554(C2) 申请公布日期 2010.09.20
申请号 RU20070141192 申请日期 2006.04.12
申请人 EHJRBAS DOJCHLAND GMBKH;DOJCHES TSENTRUM FJUR LJUFT-UND RAUMFART EH.F. (DRL) 发明人 REKZIK MARTIN;GIEBELER KRISTOF;BRJUKNER INA
分类号 B64C13/38 主分类号 B64C13/38
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