The invention discloses a countercurrent tangential type micro
turbojet engine. The countercurrent tangential type micro
turbojet engine comprises a rotor
system, a shell, a
flame tube, a diffuser, a
turbine guider, a
fuel supply system, a lubricating
system, a starting gas path and an exhaust system, wherein for the overall direction of the entire device, the position of the diffuser is defined as the left end direction of the entire device, the position of the
turbine guider is defined as the right end direction of the entire device, by taking the rotor system as the center, the diffuser is fixed at the front end of the rotor system, the
turbine guider is fixed at the right end of the rotor system, the exhaust system is positioned at the right end of the turbine guider, the
flame tube is concentric with the rotor system and contains the rotor system, the
fuel supply system and the starting gas path are fixed on the wall surface of the outer side of the
flame tube, and the lubricating system is fixed on the outer side of the rotor system, positioned between the inner side of the flame tube and the rotor system and fixed with the shell of the micro
turbojet engine through the diffuser and the turbine guider. The countercurrent tangential type micro
turbojet engine reduces the
pollutant discharge, and can effectively reduce the
carbon deposition of the flame tube, so that the
working life of the engine is prolonged.