Gas turbine fault prediction method based on kernel regeneration Hilbert space
A technology for gas turbine and fault prediction, which is applied in gas turbine engine testing, jet engine testing, neural learning methods, etc., and can solve problems such as fewer faults in the knowledge base, inability to reveal the relationship between gas turbine system components, and uncertainty in fault prediction.
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[0064] In this embodiment, a gas turbine fault prediction method based on the nuclear regeneration Hilbert space is applied to the gas turbine system, and the operating state data of m monitoring points of the gas turbine are obtained, and the operating state data of each detection point constitutes a state Vector X, denoted as X={X 1 ,X 2 ,...,X i ,...,X m}, where X i Indicates the status data of the i-th monitoring point, i∈[1,m], the purpose of this gas turbine fault prediction method is to find out the relationship between the monitoring nodes, find the monitoring node with strong correlation with any monitoring node, and in this On the basis of the method, the neural network method is used to predict the future trend of the monitoring nodes, so as to monitor the operating status of the gas turbine and warn of failures. Specifically, the gas turbine fault prediction method is carried out as follows:
[0065] Step 1. Define the candidate adjacency matrix of the state v...
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