发明名称 AIRCRAFT STRUCTURE TESTING DEVICE OF THE WIRE CUTTER TYPE
摘要 A detection wire cutter including a conducting wire mechanically secured to a structure that is to be monitored. This wire is electrically powered at one end and at another end feeds back an electrical voltage corresponding to the power supplied, provided that the structure that is to be monitored has not undergone unacceptable mechanical damage. As an improvement, two arrays of wires extending over flat supports in two directions in space are proposed. Each array is powered by a distinct network electrical supply. The two networks extend in layers, with parallel wire portions. The position of a crack does not impede the passage of current between certain terminals, but certain other terminals will no longer receive any current because the crack has broken a network supply general connection between the connection of one wire and that of another.
申请公布号 US2011231125(A1) 申请公布日期 2011.09.22
申请号 US20080811586 申请日期 2008.12.26
申请人 EUROPEAN AERONAUTIC DEFENCE AND SPACE COMPANY EADS FRANCE 发明人 ROLET SEBASTIEN;DOMINGUEZ NICOLAS
分类号 G06F19/00;G01R19/00 主分类号 G06F19/00
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