The invention relates to a hovercraft which comprises a
cockpit, a
hull, a
buoyancy tank, side walls, aprons, a gas booster, propulsion equipment, fuel equipment and
electrical control equipment, wherein the left side and the right side of the
hull are respectively provided with a side wall, and the front side and the back side of the
hull are respectively provided with an apron; the gas booster comprises a gas boosting cylinder and a gas boosting
pipe; a gas inlet is arranged at one end of the gas boosting cylinder, and a gas
inlet valve is arranged in the gas inlet; an exhaust outlet is arranged at the other end of the gas boosting cylinder, and an
exhaust valve is arranged in the exhaust outlet; an
acetylene gas inlet
pipe and an igniter are arranged on the outer surface of the gas boosting cylinder; the
detonation combustion of the
acetylene in the gas boosting cylinder generates high-pressure gas which is conveyed into a gas
cushion chamber through the gas boosting
pipe; the propulsion equipment comprises a
combustion chamber and a water
sprayer; the
combustion chamber is a cylinder body which is arranged horizontally; a gas inlet is arranged at one end of the
combustion chamber, and a gas
inlet valve is arranged in the gas inlet; an exhaust outlet is arranged at the other end of the
combustion chamber, and an
exhaust valve is arranged in the exhaust outlet; an
acetylene gas inlet pipe, an igniter and a
fuel gas pipe are arranged on the outer surface of the cylinder body; and the
detonation combustion of the acetylene in the
combustion chamber generates high-pressure
fuel gas which is conveyed into the water
sprayer through the
fuel gas pipe, thereby driving the water in the water
sprayer to flow to be spouted at a high speed from a water spout.