Fuel oil atomizing nozzle structure of turbojet engine and atomizing method thereof

The invention relates to a fuel oil atomizing nozzle structure of a turbojet engine and an atomizing method thereof, wherein the fuel oil atomizing nozzle structure of the turbojet engine comprises a mounting base, a swirler, a nozzle core, a compression channel bolt and a defoaming filter; the mounting base comprises a connecting part and a nozzle part which are sequentially arranged, the connecting part is of a cavity structure, and a plurality of evenly-distributed air holes are formed in the nozzle part; the swirler is inserted into the cavity structure, an annular cavity is formed by the swirler and the connecting part of the mounting base, and a plurality of swirling flow channels are formed in the swirler; the nozzle core is arranged between the swirler and the nozzle part, and a nozzle opening is formed in the nozzle core; the compression channel bolt is connected with the left end part of the swirler, and a plurality of first through holes are formed in the compression channel bolt; and the defoaming