发明名称 Reconfigurable integration test station
摘要 An integration test station for aircraft is provided in which the system is operable with multiple aircraft configurations. The integration test station permits aircraft component designs to be tested and verified in a simulated environment representing integration of the component into the aircraft.
申请公布号 US6269319(B1) 申请公布日期 2001.07.31
申请号 US19990240431 申请日期 1999.01.29
申请人 THE MCDONNELL DOUGLAS CORPORATION 发明人 NEISCH JONATHAN C.;TURNER DONALD E.
分类号 G01R31/00;(IPC1-7):G01R31/00;G06F19/00 主分类号 G01R31/00
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