Cutoff circuit of aeroengine ignition power supply
A technology of ignition power supply and engine, applied in the field of aviation electrical appliances
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[0007] The present invention will be described in further detail below. see figure 1 , an aeroengine ignition power cut-off circuit, comprising an engine electronic controller 1, a first ignition nozzle A and a second ignition nozzle B, the first ignition nozzle power supply output terminal 1c of the engine electronic controller 1 is connected to the first ignition nozzle A , the second ignition nozzle power supply output terminal 1d of the engine electronic controller 1 is connected to the second ignition nozzle B; it is characterized in that it also includes a double-connected single-pole normally open switch, the first relay J1 and the first relay J2; the double-connected single-pole The normally open switch is composed of the first single-pole normally open switch K1 and the second single-pole normally open switch K2; the first relay J1 has a double normally closed switch, which is composed of the first normally closed switch K3 and the second It consists of a normally cl...
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