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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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