The invention relates to a host of a
pulley block ejector, which is suitable for ejecting aircraft carrier-borne aircraft. A
piston (2) in a cylinder tube (1) is pushed by high-pressure gas, so as to drive a four-
rope pulley block to pull an ejection sliding shuttle (39) to eject the carrier-borne aircraft. The working
stroke ratio of a movable
pulley block (25) to the ejection sliding shuttle (39) is 1:4, the acceleration ratio of the movable pulley block (25) to the ejection sliding shuttle (39) is 1:4, and the acceleration
energy consumption ratio of the movable pulley block (25) to the ejection sliding shuttle (39) of equal
mass is 1:16. Four times high-speed ejection to an ejected object by using a low-speed running component is realized, and the self
mass acceleration
energy consumption is low. An eccentric outer
ring type pulley (5) is designed, and the
piston (2) is separated from a connecting rod (3), so that the
self energy consumption and the buffer braking force of the running component are greatly reduced; when the ejection sliding shuttle (39) is pulled back by an
energy storage rope from a buffer end point (44) to an ejection starting point (42) to prepare for second-time ejection, the
piston (2) is also driven to return to the
tail of the cylinder tube, so as to push the high-pressure gas into an air storage cylinder (38) and finish storing energy. The high-pressure gas can be recycled, so as not to waste energy and
fresh water like a steam ejector which uses non-expansion high-pressure hot gas once.