Energy supply system for supplying energy to aircraft systems
A technology of energy supply system and aircraft, which is applied in the direction of power system fuel cell, aircraft parts, energy-saving board measures, etc., to achieve the effect of simplifying the system
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[0036] Fig. 1 shows a simplified diagram of an energy supply system according to an exemplary embodiment of the present invention, which is used to supply electrical energy to an electrical load of an aircraft. As shown in FIG. 1, the energy supply system 100 includes a fuel cell 101, which is coupled to a capacitor 103 through a first conductive connection device or line 102. In addition, the fuel cell 101 and the capacitor 103 are coupled through a second conductive connection device 104 in which a diode 105 is interconnected. In addition, the energy supply system 100 includes a reverse rectifier 106 that is coupled to the capacitor 103 through a third conductive line 107 and a fourth conductive line 108. The voltmeter 109 is coupled between the third conductive line 107 and the fourth conductive line 108, and the voltmeter 109 is used to determine the voltage provided by the capacitor 103.
[0037] In addition, the energy supply system 100 includes a rectifier 110 that is also ...
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