发明名称 LANDING FLAP DRIVE SYSTEM
摘要 Nowadays, usually landing flap systems are used that comprise a central drive (101) with a central shaft transmission (102) to the drive stations. According to one embodiment of the present invention a landing flap drive system is stated, comprising a first drive motor (301, 302, 501) for operating a landing flap (107) . In this arrangement the landing flap drive system is essentially integrated in a track (509) of the landing flap (107) so that final assembly and integration of the system are facilitated to a significant extent.
申请公布号 CA2602667(C) 申请公布日期 2012.12.18
申请号 CA20062602667 申请日期 2006.04.12
申请人 AIRBUS DEUTSCHLAND GMBH;DEUTSCHES ZENTRUM FUER LUFT- UND RAUMFAHRT E.V. (DLR) 发明人 RECKSIEK, MARTIN;GIEBELER, CHRISTOPH;BRUECKNER, INA
分类号 B64C13/38;B64C9/16;B64C13/50 主分类号 B64C13/38
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