An Intelligent Diagnosis Method for Aeroengine Structural Faults
An aero-engine and intelligent diagnosis technology, which is applied in the direction of engine testing, machine/structural component testing, instruments, etc., can solve problems such as large input dimensions, large learning range, and dimension disasters
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[0094] Step 1: Build the fault library
[0095] Construct a fault library for the three faults of unbalance, misalignment and rotational static friction.
[0096] The purpose of the constructed fault database is to analyze the original fault data and fault phenomena of the three faults of engine unbalance, misalignment and rotational static friction, and obtain: 1. The data characteristic table of the three types of fault data; 2. The three types of fault phenomena The kinetic representation table for . Stored in the fault library.
[0097] The specific method is as follows:
[0098] Obtaining the data feature table and dynamic representation table of the three types of fault data requires two steps:
[0099] The first step is to obtain the original data of the three kinds of faults, which are the data obtained from the test system in the engine development, finalization and test.
[0100] Select the three kinds of fault original data in the early stage of reliability fluc...
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