I. Introduction
With the development of more/all electric aircrafts, the three-stage synchronous generator, widely used in current aircraft power system, has been fully considered as candidate to be integrated starter/generator due to its high safety and low cost in maintenance [1]–[3]. Fig. 1 shows the typical structure of three-stage synchronous starter/generator (TSSG) with three-phase exciter, which consists of the pre-exciter (PE), the main exciter (ME), the rotating rectifier and the main generator (MG). The PE is a permanent magnet generator which does not connect to the system in the startup process and a wound-rotor synchronous machine serves a MG. The ME is a rotating-armature electrically excited synchronous generator with three-phase field windings. Since the rotating rectifier constructs the bridge between the ME and the MG, the safety of the rotating diodes strongly affects the function of TSSG and the safety of the aircraft [4]. In addition, the failure rate of rectifier diodes is higher than other components for the influence of centrifugal force and thermal stress. Therefore, it draws high demand on the failure detection of rectifier diodes especially before the TSSG starts.
Structure of the wound-rotor synchronous starter/generator with a three-phase brushless exciter.