发明名称 ESTIMATING DYNAMIC THRUST OR SHAFT POWER OF AN ENGINE
摘要 A measuring system is provided that includes a turbine engine thrust estimator that computes "virtual measurements" of dynamic engine thrust and other parameters of interest from test cell data in a very short amount of time. The measuring system 'tunes' a user's engine model, in a numerical propulsion system simulation, by optimizing system biases and health parameters to match the sensor outputs of a set of steady state data points across the operating range. The tuned model is then utilized by the measuring system to create a constant gain extended Kalman filter that is added directly within a code of the numerical propulsion system simulation. Results, including thrust, from the numerical propulsion system simulation with Kalman filter are then presented as 'actual' corrected data.
申请公布号 WO2016133578(A2) 申请公布日期 2016.08.25
申请号 WO2015US63607 申请日期 2015.12.03
申请人 SIKORSKY AIRCRAFT CORPORATION 发明人 HETTLER, Eric Nelson;PALMER, Carl
分类号 G06F19/10 主分类号 G06F19/10
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