A dragging device for an aircraft carrier catapult
A technology of drag device and catapult, which is applied in the direction of launching/dragging transmission device, etc., which can solve the problem of not designing catapult tow rope and slider, etc., and achieve the effect of simple structure and low power consumption
Active Publication Date: 2018-11-02
马同金
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For this reason, I successively designed and invented aircraft carrier catapult energy storage flywheel and aircraft carrier energy storage flywheel transmission arm return system, the patent numbers are respectively CN201410096412.X and CN201410096413.4, but did not design the catapult towline and slider
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[0009] exist figure 1 Among them, the towing device of a kind of aircraft carrier catapult provided by the present invention, it is made up of aircraft carrier catapult energy storage flywheel, aircraft carrier energy storage flywheel transmission arm return system, annular drag belt, driving wheel, and supporting pulley, Its features are: the upper surface of the ring-shaped drag belt (1) is flush with the aircraft carrier deck (8), the ring-shaped drag belt (1) is set on the two driving wheels (2) at both ends, and the ring-shaped drag belt (1) ) There are pinch pulleys (3) outside both ends, and there is a support pulley (4) underneath; the two driving wheels (2) and the pinch pulley (3) are synchronously driven by the synchronous gear shaft (5); the synchronous gear shaft (5) Uniform acceleration and uniform deceleration are driven by the energy storage flywheel of the aircraft carrier catapult and the return system of the energy storage flywheel transmission arm of the ai...
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The invention belongs to the technical field of aircraft carrier catapults, and particularly relates to a dragging device for an aircraft carrier catapult. The dragging device for the aircraft carrier catapult is composed of an annular dragging belt, drive wheels and belt carrier wheels. The upper belt face of the annular dragging belt is flush with an aircraft carrier deck. The annular dragging belt is arranged on the two drive wheels at the two ends in a sleeving manner. Belt pressing wheels are arranged outside the two ends of the annular dragging belt, and the belt carrier wheels are arranged below the annular dragging belt. The two drive wheels and the belt pressing wheels are synchronously driven through synchronous gear shafts. The dragging device has the beneficial effects that firstly, the rotary dragging belt does not need to be braked after an airplane is catapulted, but a reciprocating sliding block vehicle needs to be urgently braked after the airplane is catapulted; secondly, the structure is simple and can be achieved in China, however, a steam catapulting structure is extremely complex and can be difficultly achieved in China; and thirdly, power consumption is small, the dragging device can be driven through conventional power, however, in the steam catapulting and electromagnetic catapulting processes, power consumption is large, and the structure can be difficultly driven through conventional power.
Description
technical field [0001] The invention belongs to the technical field of aircraft carrier catapults, in particular to a towing device for aircraft carrier catapults. Background technique [0002] The theory of the steam catapult in the United States is that there is a piston in the steam cylinder, and a towline is fixed outside the piston. The towline pulls the reciprocating slider car on the deck ejection track. On the deck of the aircraft carrier, it is also parallel to the ejection track and moves forward synchronously with the slider car; after the ejection is over, the slider car returns for the next ejection; but China has not yet mastered the specific technology of this ejection. For this reason, I have successively designed and invented aircraft carrier catapult energy storage flywheel and aircraft carrier energy storage flywheel transmission arm return system, and the patent numbers are respectively CN201410096412. Contents of the invention [0003] The technical p...
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IPC IPC(8): B64F1/06
CPCB64F1/06
Inventor 马同金
Owner 马同金