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Choice of Flight Conditions and Modes of Engine Operation for its Diagnostics

机译:诊断的飞行条件和发动机运行模式的选择

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摘要

We consider a method for diagnostics of the engine flow passage technical status of a maneuverable aircraft operating in a wide range of altitudes and speeds; the behavior of measured parameter deviations from throttle characteristics and calculated characteristics of the flow passage units from their initial values is used for diagnostics. We present the methods for determining these deviations as well as flight conditions and engine operation modes at which diagnostics is made possible.
机译:我们考虑一种用于诊断在各种高度和速度范围内运行的机动飞机的发动机流道技术状态的方法;测量的参数与节气门特性的偏差行为以及所计算的流道单元与其初始值的特性偏差的行为用于诊断。我们介绍确定这些偏差的方法,以及使诊断成为可能的飞行条件和发动机运行模式。

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