method for analyzing and evaluating a turbine engine based on a Markov dynamic fault tree
A dynamic fault tree, turbine engine technology, applied in the aviation field, can solve the problems of redundancy, low analysis and evaluation efficiency, and reduce the sufficiency of the analysis and evaluation process, and achieve the effect of reliable system evaluation results.
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[0025] Embodiment 1: as figure 1 As shown, there are 5 steps in this method, and the present embodiment takes "the amount of fuel oil supply is too large" in the numerical control system in the turbofan engine as an example.
[0026] Step1 Create a dynamic fault tree model based on the failure analysis and evaluation of the turbine engine system, create a fault tree for "excessive fuel supply", select "excessive fuel supply" as the top event of FTA, and other events are as follows: X1: in Excessive fuel supply under redundancy management failure conditions, X2: Excessive fuel supply under redundant management failure conditions, X3: Backup control cannot be activated under redundancy management failure conditions, X4: Fuel metering valve failure, system fuel supply Excessive quantity, X5: The output of the main control channel leads to excessive fuel supply, X6: The failure of the servo fuel pressure regulator leads to excessive supply, X7: The electro-hydraulic servo lubricat...
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