Research Article

Aero-Engine Fault Diagnosis Using Improved Local Discriminant Bases and Support Vector Machine

Figure 5

Aero-engine vibration signals of three different working conditions: (a) faultless, (b) rub-impact, and (c) unbalance.
283718.fig.005a
(a)
283718.fig.005b
(b)
283718.fig.005c
(c)