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Figure 17 shows the experimental acceleration of thrust pad aerostatic bearings with different types of restrictors.
The stiffness of thrust pad aerostatic bearings with different types of restrictors is shown in Figures 13, 14, 15.
Then numerical analysis of journal bearings with different dimensions is undertaken under different rotational speeds.
A series of rolling element bearings with different types of fault are experimentally studied.
3D system isolated by single-concave FPS bearings with different isolated periods in order to evaluate the potential benefits provided by increasing values of the isolation degree.
Bearings with different diameters and different rotational speeds are also studied to determine how the ultimate hydrodynamic load carrying capacity changes with diameter and rotational speed.
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The proposed method has been successfully applied in actual vibration signals of rolling element bearing with different faults.
The effectiveness of the proposed approach is demonstrated by numerical simulation and experimental investigation of rolling element bearing with different kind of faults.
The simulated vibrational response of the bearing with different local faults was used to test the suitability of the envelope analysis technique and the continuous wavelet transformation was used for the bearing-fault identification and classification.
Vibration signals from healthy bearings and bearings with three different fault locations and with three different severity levels, as well as loading conditions, are analyzed.
The experimental stiffness results of thrust pad aerostatic bearings with three different restrictor types are shown in Figure 16.
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