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.
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
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