Jet-propelled engine using discharged exhaust gas

A jet propulsion engine comprising:

• a body defining an axis;
• a combustor mounted in the body and configured to inject fuel into compressed air and combust the fuel;
• a turbine stage disposed at a rear of the combustor and configured to laterally discharge the exhaust gas at an angle of −30° to −50° relative to the axis;
• a guide member positioned downstream of the turbine stage, the guide member being configured to further laterally deflect the exhaust gas from the turbine stage to an angle of −40° to −70° relative to the axis, such that the deflected exhaust gas forms a vortex within the body;
• and
• a single propulsive force providing means positioned at a rear of the guide member and configured to provide propulsive force by colliding with the vortex of exhaust gas guided by the guide member,
• wherein the propulsive force providing means comprises:
• a rotating shaft;
• and
• a single fan blade provided at the rear of the guide member, coupled to the rotating shaft, and shaped to become more parallel to the rotating shaft toward a rear of the body, such that the exhaust gas deflected by the guide member collides with the single fan blade to produce additional thrust.