发明名称 AIRCRAFT POWER FAILURE SIMULATION APPARATUS AND METHOD
摘要 Disclosed is a flight management means verification apparatus (1) adapted to verify at least one flight management means (36,38), wherein the flight management means in use outputs a warning, disables an aircraft means and/or inhibits the activation thereof in response to a power fail condition. The flight management means verification apparatus comprises a first connection means (2,4) adapted to be disposed in a first power indicator line (74) to a first flight management means, wherein the first power indicator line provides a signal representative of a Condition of a first power supply (30), and further comprises a first switch means (14a) connected in use such that the signal of the power indicator line for the first flight management means (36) is switched. Actuating the switch means causes the signal on the power indicator line to change indicating a distortion or failure of the power supply of the aircraft and/or a part thereof. The response of the flight management means can be verified by the signal output by the flight management means, e.g. on a display, or in that the aircraft means is deactivated and/or cannot be activated.
申请公布号 US2011205089(A1) 申请公布日期 2011.08.25
申请号 US20100745248 申请日期 2010.10.19
申请人 AIRBUS OPERATIONS GMBH 发明人 KNOOP SVEN
分类号 G08B23/00 主分类号 G08B23/00
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