发明名称 DEVICE AND METHOD OF CONTROL OF POWER OF HELICOPTER ROTOR POWER PLANT
摘要 FIELD: flying vehicles power plant control systems. ^ SUBSTANCE: proposed device contains means for metering out consumption of fuel, electronic control device with means for reception of input signal corresponding to speed of rotor rotation, signal processing device with differentiator and summer, and threshold comparator. Summer is installed to determine sum of signal of rotor speed (NP) and derivative of this signal (K.dNP/dt). Threshold comparator has upper and lower thresholds, it receives output signal from summer and sends output signal to drive control mechanism. Method comes to control of power plant according to "all-or-nothings" method either for stepless increase or stepless decrease or keeping fuel delivered into engine of power plant at constant level relative to consumption of fuel at moment of failure of main control system. Control is provided as a function of speed of rotor. ^ EFFECT: simplified control in case of emergency, improved safety, reduced cost of stand-by control system. ^ 10 cl, 2 dwg
申请公布号 RU2267020(C2) 申请公布日期 2005.12.27
申请号 RU20020119582 申请日期 2000.12.18
申请人 发明人 NUSSITU KRISTIAN P'ER;MAREHN ZHAN-FILIPP ZHAK
分类号 F02C9/46;B64D31/06;F02C9/00;F02C9/28;G05D7/06;G05D13/62 主分类号 F02C9/46
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