阅读说明：本技术 一种导弹/鱼雷用支座 (Support for guided missile/torpedo ) 是由 严超亮 张义帅 王行中 王群 陈洪卫 于 2021-01-06 设计创作，主要内容包括：本发明涉及一种导弹/鱼雷用支座,包括支座本体,其前后方向开有两个方形通孔,上方为U型口,下方连接车体或固定支座的平台,上方U型口连接滚轮轴及滚轮轴卡板；支座本体底面连接弹座转接板。支座本体采用铸造后加工的方式制成；滚轮轴卡板用于固定滚轮轴左右下的移动方向；滚轮轴卡板限制滚轮轴轴向移动及向上的移动,使得滚轮轴只能沿轴心进行自转。支座本体底面通过螺纹连接弹座转接板,弹座转接板用来转接固定整体弹座的稳定,并限制其自由度。本发明的优点是,由金属铝铸造成型,熔炼和铸造工艺成熟、简单、气密性好、焊接加工性能也比较好,成型后的工件耐腐蚀性好,可适应恶劣环境,如高温、低温、湿热、盐雾较为严重环境。(The invention relates to a support for a missile/torpedo, which comprises a support body, wherein two square through holes are formed in the front and back direction of the support body, a U-shaped opening is formed in the upper part of the support body, a vehicle body or a platform for fixing the support is connected to the lower part of the support body, and a roller shaft clamping plate are connected to the U-shaped opening in the upper part of the support body; the bottom surface of the support body is connected with an elastic seat adapter plate. The support body is manufactured by adopting a casting post-processing mode; the roller shaft clamping plate is used for fixing the moving direction of the roller shaft from left to right and downwards; the roller shaft clamping plate limits the axial movement and the upward movement of the roller shaft, so that the roller shaft can only rotate along the axis. The bottom surface of the support body is connected with an elastic base adapter plate through threads, and the elastic base adapter plate is used for adapting and fixing the stability of the whole elastic base and limiting the degree of freedom of the whole elastic base. The invention has the advantages that the aluminum alloy is cast and formed by metal aluminum, the smelting and casting process is mature and simple, the air tightness is good, the welding processability is good, the formed workpiece has good corrosion resistance, and the aluminum alloy can adapt to severe environments such as high temperature, low temperature, damp heat and severe salt spray environments.)

1. A support for guided missiles/torpedoes comprises a support body (1), and is characterized in that two square through holes (2) are formed in the support body (1) in the front-back direction, a U-shaped opening (3) is formed above the support body (1), a vehicle body or a platform for fixing the support is connected below the support body (1), and the upper U-shaped opening (3) is connected with a roller shaft and a roller shaft clamping plate; the bottom surface of the support body (1) is connected with an elastic seat adapter plate.

2. A missile/torpedo support according to claim 1, wherein the support body (1) is manufactured by post-casting machining.

3. The missile/torpedo support of claim 1, wherein the roller axle clamping plate is used for fixing the moving direction of the roller axle from side to side and downwards.

4. The missile/torpedo support of claim 3, wherein the roller axle clamping plate limits axial and upward movement of the roller axle such that the roller axle is only able to spin on its axis.

5. The missile/torpedo support according to claim 1, wherein the bottom surface of the support body (1) is connected with a missile seat adapter plate through threads.

6. The missile/torpedo support of claim 5, wherein the missile mount adapter plate is used for adapting and fixing the stability of the integral missile mount and limiting the degree of freedom of the integral missile mount.

Technical Field

The invention belongs to the technical field of missile transportation process fixing, and particularly relates to a missile/torpedo support.

Background

Missile weaponry needs to be transported from production to arming troops, combat training and battlefield application, the transport environment influences the performance of the missile weaponry, and the quality of the equipment transport performance is necessarily related to the equipment reliability; the missile support in the prior art adopts bolt connection, and different environments need to be used due to uncontrollable transportation road conditions, so that the missile support runs on a bumpy road surface, the rigid connection adopts bolt connection, the phenomenon of screw loosening easily occurs for a long time, potential safety hazards are caused to transported products, and damage to missiles or other parts is possibly caused.

Disclosure of Invention

The invention aims to solve the problems and provide a missile/torpedo support which has the advantages of good casting performance, good fluidity, small linear shrinkage, low hot cracking tendency, good air tightness and excellent cutting processing performance.

In order to achieve the purpose, the invention provides the following technical scheme:

a support for guided missiles/torpedoes comprises a support body and is characterized in that two square through holes are formed in the support body in the front-back direction, a U-shaped opening is formed in the upper portion of the support body, the lower portion of the support body is connected with a vehicle body or a platform for fixing the support, and the upper U-shaped opening is connected with a roller shaft and a roller shaft clamping plate; the bottom surface of the support body is connected with an elastic seat adapter plate.

Furthermore, the support body is manufactured by adopting a casting post-processing mode.

Furthermore, the roller shaft clamping plate is used for fixing the moving direction of the roller shaft from left to right and downwards.

Furthermore, the roller shaft clamping plate limits the axial movement and the upward movement of the roller shaft, so that the roller shaft can only rotate along the axis.

Furthermore, the bottom surface of the support body is connected with an elastic seat adapter plate through threads.

Furthermore, the bullet seat keysets is used for the stability of fixed whole bullet seat of switching to restrict its degree of freedom.

Compared with the prior art, the invention has the beneficial effects that:

the invention adopts the hasp for fixed connection, and the safety device adopts the quick-release spring pin, so that the looseness and the falling off of parts in the transportation process are improved.

The missile/torpedo support is formed by casting metal aluminum, the smelting and casting process is mature and simple, the air tightness is good, the welding processing performance is good, the flaw detection process is carried out on the workpiece after the casting is finished, whether the internal structure meets the use requirement can be analyzed according to the data of a flaw detector, and the formed workpiece has good corrosion resistance and can adapt to severe environments such as high temperature, low temperature, damp heat and severe salt mist environments. The reasonability of the design according to the drawing can improve the mechanical property of the support.

Drawings

In order to more clearly illustrate the technical solution of the embodiment of the present invention, the drawings needed to be used in the description of the embodiment will be briefly introduced below, it is obvious that the drawings in the following description are only for more clearly illustrating the embodiment of the present invention or the technical solution in the prior art, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.

FIG. 1 is a schematic view of the overall structure of the present invention;

FIG. 2 is a front view of the present invention;

FIG. 3 is a left side view of the present invention;

FIG. 4 is a right side view of the present invention;

FIG. 5 is a top view of the present invention;

in the figure: 1-support body, 2-square through hole, 3-U type mouth.

Detailed Description

In order to make the technical solutions of the present invention better understood and implemented by those skilled in the art, the present invention is further described with reference to the following specific examples, which are provided for illustration only and are not intended to limit the present invention.

The missile/torpedo support shown in figures 1-5 comprises a support body 1, wherein two square through holes 2 are formed in the support body 1 in the front-back direction, and the support is used for reducing the weight, improving the reasonability of workpiece design and ensuring uniform stress.

The support body 1 is manufactured by adopting a casting post-processing mode, has extremely high requirement on the stability of the internal structure thereof and needs to be subjected to flaw detection.

The support body 1 is provided with a U-shaped opening 3 above, the U-shaped opening 3 is connected with the roller shaft and the roller shaft clamping plate, and the roller shaft clamping plate limits the axial movement and the upward movement of the roller shaft for fixing the movement of the roller shaft in three directions, namely left, right and down, so that the roller shaft can only rotate along the axis.

The lower part of the support body 1 is connected with a vehicle body or a platform for fixing the support, thereby limiting the movement of the support in all directions.

The bottom surface of the support body 1 is connected with an elastic base adapter plate, and the connection mode adopts threaded connection and is used for adapting and fixing the stability of the whole elastic base and limiting all the degrees of freedom of the whole elastic base.

The invention adopts the hasp for fixed connection, and the safety device adopts the quick-release spring pin, so that the looseness and the falling off of parts in the transportation process are improved.

The missile/torpedo support is formed by casting metal aluminum, the smelting and casting process is mature and simple, the air tightness is good, the welding processing performance is good, the flaw detection process is carried out on the workpiece after the casting is finished, whether the internal structure meets the use requirement can be analyzed according to the data of a flaw detector, and the formed workpiece has good corrosion resistance and can adapt to severe environments such as high temperature, low temperature, damp heat and severe salt mist environments. The reasonability of the design according to the drawing can improve the mechanical property of the support.

The details of the present invention not described in detail are prior art.

The above description is only for the purpose of illustrating the preferred embodiments of the present invention and is not to be construed as limiting the invention, and any modifications, equivalents, improvements and the like that fall within the spirit and principle of the present invention are intended to be included therein.