发明名称 Advanced aircraft instrumentation apparatus
摘要 An apparatus for installing, at the front end of an instrument panel, an aircraft instrument having a rectangular chassis. The installation occurs by advancing a screw through a corner adaptor, into the instrument. The adaptors are attached to the periphery of a rectangular hole in the instrument panel, after the instrument has been inserted therethrough, so as to create an octagonal hole as is typically found in instrument panels. The corner adaptors are made up of a first plate and a second plate having a spacer region which is slightly narrower than the thickness of the instrument panel. When a screw is inserted through the first plate and the second plate, they are held together and adhere to the instrument panel which is inserted therein.
申请公布号 US4913383(A) 申请公布日期 1990.04.03
申请号 US19880272155 申请日期 1988.11.16
申请人 ROCKWELL INTERNATIONAL CORPORATION 发明人 HILL, RICHARD T.;HEIDT, ROGER W.
分类号 B64D43/00 主分类号 B64D43/00
代理机构 代理人
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