发明名称 Engine Vibration and Engine Trim Balance Test System, Apparatus and Method
摘要 <p>The present disclosure is generally directed to a simulated aircraft engine (12) accelerometer apparatus, system and method that that generates aircraft engine (12) simulator outputs. An accelerometer signal simulator (320) receives aircraft engine (12) simulator outputs and generates accelerometer signal simulator (320) outputs, and an accelerometer waveform generator (350) receives the accelerometer signal simulator (320) outputs and synchronizes at least one accelerometer signal simulator (320) outputs to a reference timing signal from one of the aircraft engine (12) simulator outputs. The simulated accelerometer (300) further includes a filter section (372, 374, 376 and 378) that receives and filters noise from the plurality of accelerometer waveform generator (350) outputs to generate a plurality of filtered accelerometer waveform generator (350) outputs, a mixer (380) that receives and combines each of the plurality of filtered accelerometer waveform generator (350) outputs to generate a single filtered accelerometer waveform generator (350) output, and a charge converter (382) that receives and converts the single filtered accelerometer waveform generator (350) output to a current charge vibration simulation output.</p>
申请公布号 EP2674741(A1) 申请公布日期 2013.12.18
申请号 EP20130170892 申请日期 2013.06.06
申请人 THE BOEING COMPANY 发明人 SCHWAB, ROBERT B;PHAM, GIANG Q.;KLINGMAN, JAN DONALD
分类号 G01M15/12;G01M15/02 主分类号 G01M15/12
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