The invention discloses a pre-combusted aircraft engine 
plasma igniter. The pre-combusted aircraft engine 
plasma igniter comprises an outer tube, a 
ceramic tube fuel channel, a 
cathode portion, an 
anode, an insulation sleeve, a 
bushing and a top cover; the 
cathode portion is installed on the middle-lower portion of the 
ceramic tube fuel channel in a sleeving mode, and a 
nozzle is arranged at the front end of the 
ceramic tube fuel channel; the insulation sleeve is installed on the middle-upper portion of the 
cathode portion in a sleeving mode and arranged in the outer tube; air inlet holes areformed in the outer wall of the lower portion of the outer tube, the 
anode is arranged under the air inlet holes, the upper portion of the 
anode is located in the outer tube and is in threaded connection with the outer tube, and the anode is a hollow revolving body; the cathode portion comprises a cathode base and a cathode, the upper portion of the cathode is in threaded connection with the lowerportion of the cathode base, and a spiral groove is formed in the middle of the inner wall of the anode; the lower end of the 
bushing is fixedly connected with the upper end of the cathode base; andthe top cover is installed outside the 
bushing in a sleeving mode, and the lower portion of the top cover is fixedly connected with the upper end of the outer tube. According to the pre-combusted aircraft engine 
plasma igniter, the ceramic tube fuel channel is additionally installed in the cathode portion, a reaction occurs outside the anode, therefore, electrodes are protected, the safety is improved, and the insulating problem is well solved.