发明名称 |
ADAPTIVE FLAP AND SLAT DRIVE SYSTEM FOR AIRCRAFT |
摘要 |
A drive station includes two drives connected via drive transmissions to one or more flaps or slats of a flap/slat group. The drives may be mechanically coupled to a rotational shaft, with a shaft brake arranged thereon. Guide transmissions are connected to the shaft and to respective flaps or slats of the flap/slat group. Alternatively, the two drives are not mechanically coupled, but are merely electrically or electronically synchronized. Each flap/slat group can be actuated individually and independently of the other groups by actuation commands provided by a central control unit connected to the drives and to a flight controller. Position sensors provide actual position feedback. Each flap/slat is driven by two transmissions, namely two drive transmissions, or two guide transmissions, or one drive transmission and one guide transmission. A redundant drive path is ensured if a component fails.
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申请公布号 |
CA2462217(A1) |
申请公布日期 |
2004.09.27 |
申请号 |
CA20042462217 |
申请日期 |
2004.03.29 |
申请人 |
BESING, WOLFGANG;RECKSIEK, MARTIN;RECHTER, HARALD |
发明人 |
BESING, WOLFGANG;RECKSIEK, MARTIN;RECHTER, HARALD |
分类号 |
B64C13/00;B64C3/00;B64C13/50;B64D45/00;(IPC1-7):B64C13/38;B64C9/16 |
主分类号 |
B64C13/00 |
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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