Gear fault diagnosis method based on ESMF and energy operator demodulation
An energy operator demodulation and fault diagnosis technology, applied in the testing of machine gear/transmission mechanism, measuring device, testing of mechanical components, etc. frequency and other issues, to achieve the effect of good demodulation effect and small calculation amount
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Embodiment 1
[0076] S1. Using an acceleration sensor to measure the vibration of the gear box to obtain an acceleration signal of the gear vibration.
[0077] Build an experimental device for simulating gear faults. The schematic diagram of the gear box structure is shown in image 3 As shown, gear 1 is the driving gear, and gear 2 is the driven gear. One tooth of gear 2 is artificially cut, and gear 1 is normal, so as to simulate a gear broken tooth fault. gear 1 tooth number z 1 =55, gear 2 tooth number z 2 =75, modulus m=2, install the acceleration sensor on the gear box body, collect the gear vibration signal, the sampling frequency is 3600Hz, the sampling time is 1 second, and the output shaft (axis II) rotates at a speed of 820r / min The next step is to collect a group of vibration signals under the condition of broken teeth of gears. The collected vibration acceleration signal in the case of gear failure is x p (t), such as Figure 4 shown.
[0078] From the known conditions ab...
Embodiment 2
[0094] S1. Using an acceleration sensor to measure the vibration of the gear box to obtain an acceleration signal of the gear vibration.
[0095] Replace the gear 2 with the same normal gear, and the rest of the parameter settings are the same as in the first embodiment, and the vibration acceleration signal of the measured gear under normal conditions is x q (t), such as Figure 8 shown.
[0096] S2. Perform extremum point symmetric mode decomposition on the acceleration signal of gear vibration to obtain several IMF components and a residual component.
[0097] For vibration signal x q (t) Carry out extreme point symmetric mode decomposition to obtain 4 IMF components, denoted as (c 1 (t),c 2 (t),c 3 (t),c 4 (t)), and a residual component, denoted as r 4 (t).
[0098] S3, using the energy operator demodulation method to the first two IMF components c 1 (t), c 2 (t) Demodulate and estimate the envelope signals of the two IMF components.
[0099] S4. Draw the amplit...
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