发明名称 Aircraft lift augmentation system with overload protection
摘要 The operating drive has a central drive system, coupled to elements for transmission of the drive energy over the full width of the wing to individual drive stations (10) for the different landing flaps. Overload protection is provided by a number of electrical load sensors, associated with the points of transmission of the drive energy to the operating drives for the flap bodies.
申请公布号 EP1452442(A1) 申请公布日期 2004.09.01
申请号 EP20040003823 申请日期 2004.02.19
申请人 LIEBHERR-AEROSPACE LINDENBERG GMBH 发明人 SCHIEVELBUSCH, BERND
分类号 B64C9/16;B64C13/24;(IPC1-7):B64C13/24 主分类号 B64C9/16
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