发明名称 Engine Vibration And Engine Trim Balance Test System, Apparatus And Method
摘要 The present disclosure is generally directed to a simulated aircraft engine accelerometer apparatus, system and method that that generates aircraft engine simulator outputs. An accelerometer signal simulator receives aircraft engine simulator outputs and generates accelerometer signal simulator outputs, and an accelerometer waveform generator receives the accelerometer signal simulator outputs and synchronizes at least one accelerometer signal simulator outputs to a reference timing signal from one of the aircraft engine simulator outputs. The simulated accelerometer further includes a filter section that receives and filters noise from the plurality of accelerometer waveform generator outputs to generate a plurality of filtered accelerometer waveform generator outputs, a mixer that receives and combines each of the plurality of filtered accelerometer waveform generator outputs to generate a single filtered accelerometer waveform generator output, and a charge converter that receives and converts the single filtered accelerometer waveform generator output to a current charge vibration simulation output.
申请公布号 US2013338982(A1) 申请公布日期 2013.12.19
申请号 US201213495447 申请日期 2012.06.13
申请人 SCHWAB ROBERT B.;KLINGMAN JAN DONALD;PHAM GIANG 发明人 SCHWAB ROBERT B.;KLINGMAN JAN DONALD;PHAM GIANG
分类号 G06G7/70 主分类号 G06G7/70
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