| 摘要 |
A method for achieving linear engine thrust response comprising the steps of measuring a throttle position (FNRQ), measuring a plurality of engine parameters, inputting the plurality of engine parameters and the throttle position into a pluralit y of schedules to produce a plurality of outputs, combining the plurality of outputs to produc e a part power scheduled airflow (W2RSCH), and using the W2RSCH to produce a near linear thrust response of the engine.
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