Missile tail blade closing machine

Abstract

The invention relates to a blade folding device, in particular to a guided missile tail blade folding machine. The guided missile tail blade folding machine comprises an upper support, a lower support, a blade screwing device, a first guide rail, a first sliding block, a holding device, a compression device and an air cylinder; the upper support is arranged on the lower support, and the lower support is provided with the blade screwing device used for screwing missile tail blades; the upper support is provided with the compression device used for downwards pressing a missile body and the holding device used for holding the blades, and the holding device is located between the blade screwing device and the compression device; and the first guide rail is installed on the upper support in the vertical direction, the holding device is in sliding connection with the first guide rail through the first sliding block, the air cylinder is arranged at the top of the upper support, and the output end of the air cylinder is connected with the holding device. The guided missile tail blade folding machine is reasonable and compact in structure and reliable in performance, the blade screwing efficiency is improved, the manual labor strength is reduced, and obvious deformation and appearance damage of the blades in the screwing process are avoided.

Description

technical field [0001] The invention relates to a blade folding device, in particular to a missile tail blade folding machine. Background technique [0002] The missile includes the front and rear sections of the nozzle, the cylinder, and the blades. The cylinder with the blades can rotate relative to the front and rear sections of the nozzle. At present, there is no fully automatic blade closing equipment for this structure. At present, the production process is mainly done manually. When closing, it is necessary to install gaskets on each blade, and close the blades one by one, and then fix the product blades with ropes and cover the protective ring, which is not only slow in efficiency, but also drags The entire production rhythm, and the physical energy consumption of the workers is also relatively large. When the blades are closed manually, it is inevitable to damage the blades. Contents of the invention [0003] In view of the above problems, the purpose of the pres...

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Problems solved by technology

[0003] In view of the above problems, the object of the present invention is to provide a missile tail blade closing machine to solve the problems of low work efficiency and large damage to the blades in the prior art when the blades are closed manually

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