The invention provides a pneumatic type ejector for carrier-based airplanes of an
airplane carrier. A group of steel wire ropes are driven to shrink by a plurality of closed pneumatic cylinders at the same time, and a sliding shuttle on a
takeoff runway is driven to slide through the shrinkage of the steel wire ropes, so that the carrier-based airplanes are pushed to take off in an ejecting mode. The structure comprises the carrier-based
airplane takeoff runway, the sliding shuttle, the traction steel wire ropes, a plurality of
pneumatic cylinder module components, high-pressure gas pipes and a resetting
winch, wherein the
pneumatic cylinder module components consist of fixed frameworks, the pneumatic cylinders, pistons,
piston connecting rods,
pulley frames, driving pulleys, anti-breaking pulleys and sliders; the cylinder bodies of the pneumatic cylinders are fixed in the fixed frameworks; the
head parts of the pneumatic cylinders are arranged at intervals in a staggered and opposite mode; and the
tail parts of the pneumatic cylinders are connected with the high-pressure gas pipes by electrically-controlled valves. Compared with the prior art, the large-thrust multiple acceleration type pneumatic ejector for the carrier-based airplanes of the
airplane carrier is characterized in that: the large-thrust multiple acceleration type pneumatic ejector has a simple structure, low cost, light weight, a high power conversion rate and long service life, saves energy and can adapt to the launch of various carrier-based airplanes (including light aircrafts and unmanned aerial vehicles), and the power and the
takeoff distance can be adjusted.