Real-time judging method and real-time judging system for aircraft engine test safety parameter monitoring
An aero-engine and safety parameter technology, which is applied in the direction of engine testing, machine/structural component testing, and measuring devices, can solve problems such as heavy losses, high R&D costs, and difficulty in ensuring engine safety, and achieve the effect of simple structural design
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[0027] The real-time discrimination method of aero-engine test safety parameter monitoring of the present invention, the specific process is:
[0028] S010. Establish a multi-dimensional steady-state rated data table based on key parameters related to engine safety; the multi-dimensional steady-state rated data table includes inlet temperature, inlet pressure, ambient pressure, cross-section, rated speed, variables, and rated values.
[0029] S020. From the rated data table, according to a certain calculation method, calculate the rated value of the safety parameter in the transition process in real time;
[0030] S030. On the basis of the steady-state rated data table, determine the safety upper limit and lower limit of each parameter under corresponding conditions;
[0031] S040. Provide a value selection rule for a real-time safety parameter upper limit and a lower limit of the transition process, where the value is obtained from the rated value of the safety parameter in t...
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