CN108398052B

CN108398052B - Variable caliber rocket launching director

Info

Publication number: CN108398052B
Application number: CN201810479918.7A
Authority: CN
Inventors: 龚毅; 邹春根; 顾春涛; 朱科平; 王雪霖; 常江; 杨宏伟
Original assignee: Xinyu Guoke Special Equipment Co ltd
Current assignee: Xinyu Guoke Special Equipment Co ltd
Priority date: 2018-05-18
Filing date: 2018-05-18
Publication date: 2024-09-17
Anticipated expiration: 2038-05-18
Also published as: CN108398052A

Abstract

The invention provides a variable caliber multi-joint rocket launching director, which comprises a frame body, a bullet baffle, an upper guide rail, a lower guide rail, a connecting rod, a lifting device and a handle, wherein the frame body is provided with a plurality of grooves; the bullet blocking device is arranged at one end of the lower guide rail, the lifting device is arranged at the upper end of the frame body through a connecting piece, the lifting device is in transmission connection with the upper guide rail through a connecting rod, and the lower guide rail is arranged at the lower end of the frame body. The effect of it is that: 1. the flexibility of operation is improved, and the use cost is reduced. 2. The processing and assembling difficulty is reduced. 3. The transmitting caliber has wide adjusting range, is simple and convenient, and has the functions of self locking and position locking.

Description

Variable caliber rocket launching director

Technical field:

the invention relates to an improved civil rocket launching device, in particular to a variable caliber rocket launching director.

The background technology is as follows:

The existing rocket launcher orienter, see figures 1 and 2, is characterized in that the caliber is fixed, the adjustment is difficult, and only one caliber rocket launching requirement can be met. The rocket launching device has the following defects in use: 1. the adaptability is poor, and the requirements of the existing market on launching rockets with various calibers cannot be met; 2. the running cost of enterprises is high, because rockets with different calibers are required to be matched with corresponding launching directors, under the requirement of multi-caliber rocket launching, the enterprises are required to be matched with a plurality of launching directors with different calibers, which definitely leads the running cost of the enterprises to be high; 3. in the case of multi-caliber rocket launch, the operation is inconvenient because a plurality of launch directors with different calibers are needed.

The invention comprises the following steps:

The invention aims to overcome the defects of the existing rocket launcher orienter and provides a variable caliber multi-combined rocket launcher orienter, wherein the caliber of the variable caliber multi-combined rocket launcher orienter can be adjusted within a range.

The invention can realize the aim through the following technical scheme, and is characterized by comprising a frame body, a bullet blocking device, an upper guide rail, a lower guide rail, a connecting rod, a lifting device and a handle; the bullet blocking device is arranged at one end of the lower guide rail, the lifting device is arranged at the upper end of the frame body through a connecting piece, the lifting device is in transmission connection with the upper guide rail through a connecting rod, and the lower guide rail is arranged at the lower end of the frame body.

The lifting device is formed by connecting a worm and a worm wheel connecting rod in a transmission way, and one end of the worm is provided with a handle jack.

The bullet blocking device consists of a bullet blocking cover, a spring and a bullet blocking tongue, wherein the spring and the bullet blocking tongue are sequentially arranged in the bullet blocking cover, and the bullet blocking cover is fixed on the lower guide rail.

For being used for being connected with rocket launcher main part, be equipped with the adapter block on the support body, be equipped with star handle screw on the adapter block.

The frame body is provided with an aviation socket for accessing an ignition power supply, and is also provided with a binding post for outputting ignition, and the binding post is connected with the aviation socket through a wire.

In order to protect the worm, a worm cover plate is arranged on the worm.

In order to prevent the upper guide rail from moving left and right, the connecting piece is provided with a guide groove.

The invention has the following effects: 1. the flexibility of operation is improved, and the use cost is reduced, and the device is adjustable in caliber, wide in adjusting range, and free from carrying directors with different calibers, and a user can adjust the caliber according to requirements. 2. The processing and assembling difficulty is reduced, the fixed caliber director has extremely high processing and assembling requirements, otherwise, the rocket launching requirement cannot be met, the caliber of the device is adjustable, and the processing and assembling requirements are reduced. 3. The transmitting caliber adjusting range is wide, the device is simple and convenient, has self-locking and position locking functions, and can adjust the transmitting caliber of any channel by using a special tool.

Description of the drawings:

FIG. 1 is a schematic diagram of a prior art front view structure;

fig. 2 is a schematic diagram of a left-hand structure of the prior art.

FIG. 3 is a schematic view (enlarged) of the front view structure of the present invention;

FIG. 4 is a schematic left-hand view (enlarged) of the present invention;

FIG. 5 is a schematic right-side view (enlarged) of the present invention;

FIG. 6 is an enlarged schematic view of the lifting device of FIG. 3;

FIG. 7 is an enlarged schematic view of the bullet stop of FIG. 3;

fig. 8 is a schematic view of the structure of the handle in the present invention.

The specific embodiment is as follows:

Referring to fig. 1,2, 3,4, 5,6, 7 and 8, a variable caliber multi-joint rocket launching director mainly comprises a frame body 1, a bullet baffle 2, an upper guide rail 3, a lower guide rail 4, a connecting rod 5, a lifting device 6, a handle 7, a connecting piece 9, an adapter 10, a star-shaped handle screw 11, a binding post 12 and an aviation socket 13. The bullet blocking device 2 is arranged at one end of the lower guide rail 4. The lifting device 6 fixes the upper end of the frame body 1 through a connecting piece 9. The lifting device 6 is in transmission connection with the upper guide rail 3 through a connecting rod 5. The lower guide rail 4 is arranged at the lower end of the frame body 1, and the connecting part is provided with a concave-convex groove for convenient assembly. The lifting device 6 is formed by connecting a worm 61 and a worm gear connecting rod 62 in a transmission way, one end of the worm 61 is provided with a handle 8 jack 63, and in order to protect the worm 61, a worm cover plate 64 is arranged on the worm 61, and the worm cover plate 64 is in interference fit. The bullet blocking device 2 consists of a bullet blocking cover 21, a spring 22 and a bullet blocking tongue 23, wherein the spring 22 and the bullet blocking tongue 23 are sequentially arranged in the bullet blocking cover 21, the bullet blocking cover 21 is fixed on the lower guide rail 4, and when a rocket enters from the rear part of a channel during loading, the bullet blocking tongue 23 is compressed, and the rocket is completely prevented from falling off after entering the back bullet blocking tongue 23. For being used for being connected with rocket launcher main part, be equipped with the adapter piece 10 on the support body 1, be equipped with star handle screw 11 on the adapter piece 10. The frame body 1 is provided with an aviation socket 13 for accessing an ignition power supply, and is also provided with a binding post 12 for outputting ignition, and the binding post 12 is connected with the aviation socket 13 by a wire. In order to prevent the upper guide rail 3 from moving laterally, the connecting member 9 is provided with a guide groove.

The principle and the operation flow of the device are as follows: the lower guide rail 4 supports the rocket, and the upper guide rail 3 is positioned to form a launching channel together. The upper guide rail 3, the worm wheel connecting rod 62 and the connecting rod 5 form a parallelogram structure, when the caliber needs to be adjusted, the handle 7 is inserted into the insertion hole 63, the worm 61 is rotated, the worm wheel connecting rod 62 is driven to rotate, and the upper guide rail 3 moves up and down, so that the caliber adjusting purpose is achieved.

Claims

1. The variable caliber multi-joint rocket launching director is characterized by comprising a frame body, a bullet baffle, an upper guide rail, a lower guide rail, a first connecting rod, a lifting device and a handle; the bullet blocking device is arranged at one end of the lower guide rail, the lifting device is arranged at the upper end of the frame body through the connecting piece, and the lower guide rail is arranged at the lower end of the frame body; the lifting device is formed by connecting a worm and a worm gear connecting rod in a transmission way, and a handle jack is formed at one end of the worm; the worm gear connecting rod consists of a worm gear and a second connecting rod, one end of the second connecting rod is fixed with the worm gear, the other end of the second connecting rod is rotationally connected with the upper guide rail, and one end of the first connecting rod is rotationally connected with the upper guide rail; the upper guide rail, the worm gear connecting rod and the first connecting rod form a parallelogram structure; the bullet blocking device consists of a bullet blocking cover, a spring and a bullet blocking tongue, wherein the spring and the bullet blocking tongue are sequentially arranged in the bullet blocking cover, and the bullet blocking cover is fixed on the lower guide rail; the frame body is provided with a switching block, and the switching block is provided with a star-shaped handle screw; the frame body is provided with an aviation socket for accessing an ignition power supply, and is also provided with a binding post for outputting ignition, and the binding post is connected with the aviation socket by a wire; a worm cover plate is arranged on the worm; the connecting piece is provided with a guide groove.