发明名称 Rotating round dial aircraft engine instruments
摘要 An apparatus and method for displaying an engine performance parameter are provided wherein the scale for reading the value of the engine performance parameter is rotated as required in order that a pointer showing the value of the engine performance parameter appears at a desired clock position on a display when the value of the engine performance parameter is equal to a predetermined value, such as a takeoff thrust value.
申请公布号 US5404766(A) 申请公布日期 1995.04.11
申请号 US19920955074 申请日期 1992.10.01
申请人 HONEYWELL INC. 发明人 THOMAS, HAROLD W.
分类号 B64D43/00;G01D7/02;(IPC1-7):G01D7/02 主分类号 B64D43/00
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