发明名称 Self-sufficient control unit for externally checking the operation of an aircraft landing gear
摘要 An autarkic control unit including a protection switch, voltage controller (2) a two-pole selector switch (3) with three switch-positions, three time delay units (4), two piezo-signal transmitters (5) and three actuating keys (6) with returning action, is designed to enable externally controlled autarkic testing of an under-carriage, including the undercarriage hinged-covers, function, independently and in parallel with the on-going systems testing at the in-board aircraft panel, with actuation of undercarriage covers, and the raising and lowering of the undercarriage accompanied by an acoustic warning before and during autarkic testing so as to avoid injury to personnel. The first switch output corresp. to the first position of the selector switch (3) is connected to the first input of a second time-delay unit (4.2), which occupies one switch contact, and a second switch output corresp. to the selector switch (3) second position is connected to the first input of a first time-delay unit (4.1), occupying a first switch contact.
申请公布号 EP0739817(A3) 申请公布日期 1997.11.05
申请号 EP19960103616 申请日期 1996.03.08
申请人 DAIMLER-BENZ AEROSPACE AIRBUS GESELLSCHAFT MIT BESCHRAENKTER HAFTUNG 发明人 HEIL, LEONHARD
分类号 B64D45/04;B64F5/00 主分类号 B64D45/04
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