阅读说明：本技术 一种导弹及炸弹的支撑固定装置 (Supporting and fixing device for guided missile and bomb ) 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及炸弹的支撑固定装置,包括弹支座及框式横梁,框式横梁上开有定位孔,弹支座整体固定在该定位孔中,弹支座底部设有弹座转接板及若干定位销,定位销插入框式横梁中,弹座转接板底部通过连接件将其与框式横梁连接起来；弹支座两侧设有相互配合连接的弹座挂钩板及搭扣锁,用于固定放置在弹支座滚轮组件顶部的弹体。弹座挂钩板及搭扣锁通过帆布袋压板及帆布袋分别固定在弹支座两侧；帆布袋压板中间位置设有防静电胶皮；弹支座前后两面均设有搭扣锁。本发明的优点是,帆布袋上的防静电胶皮与弹体表面接触,增大摩擦力,防止弹体的转动。(The invention relates to a supporting and fixing device for a guided missile and a bomb, which comprises a missile support and a frame-type beam, wherein the frame-type beam is provided with a positioning hole, the missile support is integrally fixed in the positioning hole, the bottom of the missile support is provided with a missile support adapter plate and a plurality of positioning pins, the positioning pins are inserted into the frame-type beam, and the bottom of the missile support adapter plate is connected with the frame-type beam through a connecting piece; the two sides of the bullet support are provided with a bullet seat hook plate and a hasp lock which are mutually matched and connected, and the bullet seat hook plate and the hasp lock are used for fixing a bullet body placed at the top of the bullet support roller assembly. The elastic seat hook plate and the hasp lock are respectively fixed on two sides of the elastic support through the canvas press plate and the canvas; an anti-static rubber is arranged in the middle of the canvas bag pressing plate; the front and the back surfaces of the elastic support are provided with hasp locks. The invention has the advantages that the anti-static rubber on the canvas bag is contacted with the surface of the projectile body, so that the friction force is increased, and the rotation of the projectile body is prevented.)

1. A supporting and fixing device for guided missiles and bombs comprises a missile support (1) and a frame-type beam (12), and is characterized in that the frame-type beam (12) is provided with a positioning hole (13), the missile support (1) is integrally fixed in the positioning hole (13), the bottom of the missile support (1) is provided with a missile seat adapter plate (19) and a plurality of positioning pins (15), the positioning pins (15) are inserted into the frame-type beam (12), and the bottom of the missile seat adapter plate (19) is connected with the frame-type beam (12) through a connecting piece (14);

the bullet support (1) both sides are equipped with bullet seat couple board (8) and hasp lock (9) of mutually supporting connection for fix place bullet body (2) at bullet support roller components (6) top.

2. A missile and bomb supporting and fixing device as claimed in claim 1, wherein the missile seat hook plate (8) and the hasp lock (9) are respectively fixed on both sides of the missile support seat (1) through a canvas pressing plate (4) and a canvas (5).

3. A missile and bomb supporting and fixing device as claimed in claim 2, wherein the canvas bag pressing plate (4) is provided with an antistatic rubber (10) at the middle position.

4. A missile and bomb supporting and fixing device as claimed in claim 1, characterised in that the hasp lock (9) is provided with a hasp handle (11) and a spring pin (3).

5. Missile and bomb supporting and fixing device according to claim 1, characterised in that the connecting piece (14) is a bolt and a self-locking nut or a double nut which are connected in a matching way.

6. A missile and bomb support fixing device in accordance with any one of claims 1 to 5 characterised in that the missile support (1) is provided with snap locks on both the front and back sides.

7. The missile and bomb supporting and fixing device as claimed in claim 6, wherein the hasp lock comprises a hasp base (18) and a hasp handle (11) fixed on the hasp base (18), and the hasp base (18), the hasp handle (11) and a hook T-shaped stud (17) are coaxially connected through a fastening bolt below the hasp base (18); and a hook ring nut (20) and a second hook plate (16) are sequentially connected below the hook T-shaped stud (17).

8. A missile and bomb supporting and fixing device as claimed in claim 7, wherein the hook T-shaped stud (17) is connected with the pin washer and the hasp handle (11) through a pin shaft, and the hook T-shaped stud (17) rotates within an effective range.

9. The missile and bomb supporting and fixing device as claimed in claim 7, wherein the hasp base (18) is connected with a hasp adapter plate or a door plate fixing plate through a countersunk screw, and a canvas bag adapter plate is additionally arranged in the middle of the hasp base (18) and the hasp adapter plate when the hasp base is fixed.

Technical Field

The invention belongs to the technical field of projectile body fixing devices, and particularly relates to a supporting and fixing device for a guided missile and a bomb.

Background

Missile weaponry needs to pass through the transportation process from production to equipment units and task training, the transportation environment influences the performance of the missile weaponry, and the good and bad of the equipment transportation performance are necessarily related to the equipment reliability; the transportation mode comprises personnel carrying, vehicle transportation, ship transportation, air transportation and air delivery, and the research on the transportation performance of the missile weaponry has practical significance.

Disclosure of Invention

The invention aims to solve the problems and provide a missile and a bomb supporting and fixing device which increase friction force and prevent a missile body from rotating.

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

a supporting and fixing device for guided missiles and bombs comprises a missile support and a frame-type beam, and is characterized in that the frame-type beam is provided with a positioning hole, the missile support is integrally fixed in the positioning hole, the bottom of the missile support is provided with a missile seat adapter plate and a plurality of positioning pins, the positioning pins are inserted into the frame-type beam, and the bottom of the missile seat adapter plate is connected with the frame-type beam through a connecting piece;

the two sides of the bullet support are provided with a bullet seat hook plate and a hasp lock which are mutually matched and connected, and the bullet seat hook plate and the hasp lock are used for fixing a bullet body placed at the top of the bullet support roller assembly.

Further, the elastic seat hook plate and the hasp lock are fixed on two sides of the elastic support through the canvas press plate and the canvas respectively.

Furthermore, an anti-static rubber is arranged in the middle of the canvas press plate.

Furthermore, a hasp handle and a spring pin are arranged on the hasp lock.

Furthermore, the connecting piece is a bolt and a self-locking nut or a double nut which are connected in a matched mode.

Furthermore, the front and the rear surfaces of the elastic support are provided with snap locks.

Furthermore, the hasp lock comprises a hasp base and a hasp handle fixed on the hasp base, and the hasp base, the hasp handle and the hook T-shaped stud are coaxially connected through a fastening bolt below the hasp base; and a hook ring nut and a second hook plate are sequentially connected below the hook T-shaped stud.

Furthermore, the hook T-shaped stud is connected with the pin shaft gasket and the hasp handle through a pin shaft, and the hook T-shaped stud rotates within an effective range.

Furthermore, the hasp base is connected with the hasp adapter plate or the door plate fixing plate through a countersunk screw, and the middle of the hasp base is additionally provided with the canvas adapter plate when the hasp base is fixed with the hasp adapter plate.

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

the invention places the projectile body on the projectile support assemblies at the positions a and b, the pivot position needs to be consistent with the projectile body pivot position, the projectile body is directly placed on the projectile support assemblies to rotate, the sailcloth bag is wound on the surface of the projectile body, the quick-release spring pin is pulled out, the hasp ring nut is adjusted to be tightly buckled with the hook plate, the hasp handle is pushed downwards, the hook plate is tightly buckled with the hasp ring nut, the anti-static rubber on the sailcloth bag is contacted with the surface of the projectile body, the friction force is increased, the quick-release spring pin is inserted, and the rotation of the projectile body is prevented.

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 schematic representation of the use of the present invention;

FIG. 3 is a schematic structural view of the adapter plate of the spring seat of the present invention;

in the figure: 1-elastic support, 2-elastic body, 3-spring pin, 4-canvas press plate, 5-canvas, 6-roller component, 8-hook plate, 9-hasp lock, 10-antistatic rubber, 11-hasp handle, 12-frame beam, 13-positioning hole, 14-connecting piece, 15-positioning pin, 16-second hook plate, 17-hook T-shaped stud, 18-hasp base, 19-elastic base adapter plate and 20-hasp ring nut.

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 and bomb supporting and fixing device shown in fig. 1-3 comprises a bomb support 1 and a frame-type beam 12, wherein a positioning hole 13 is formed in the frame-type beam 12, the bomb support 1 is integrally fixed in the positioning hole 13, a bomb seat adapter plate 19 and a plurality of positioning pins 15 are arranged at the bottom of the bomb support 1, the positioning pins 15 are inserted into the frame-type beam 12, and the bottom of the bomb seat adapter plate 19 is connected with the frame-type beam 12 through a connecting piece 14; the two sides of the bullet support 1 are provided with a bullet support hook plate 8 and a hasp lock 9 which are mutually matched and connected, and the bullet support hook plate and the hasp lock 9 are used for fixing the bullet bodies 2 placed at the top of the bullet support roller assembly 6; the elastic seat hook plate 8 and the hasp lock 9 are respectively fixed on two sides of the elastic support 1 through the canvas press plate 4 and the canvas 5. An anti-static rubber 10 is arranged in the middle of the canvas bag pressing plate 4; the hasp lock 9 is provided with a hasp handle 11 and a spring pin 3.

The front surface and the rear surface of the elastic support seat 1 are respectively provided with a hasp lock, the hasp lock comprises a hasp base 18 and a hasp handle 11 fixed on the hasp base 18, and the hasp base 18, the hasp handle 11 and a hook T-shaped stud 17 are coaxially connected through a fastening bolt below the hasp base 18; and a hook ring nut 20 and a second hook plate 16 are sequentially connected below the hook T-shaped stud 17.

The hook T-shaped stud 17 is connected with the pin shaft gasket and the hasp handle 11 through a pin shaft, and the hook T-shaped stud 17 rotates within an effective range. The hasp base 18 is connected with a hasp adapter plate or a door plate fixing plate through countersunk screws, and a canvas adapter plate is additionally arranged in the middle of the hasp base 18 and the hasp adapter plate when the hasp base is fixed.

Preferably, the connecting member 14 is a bolt and a self-locking nut or a double nut which are connected in a matching manner.

The using method of the invention comprises the following steps:

according to the known fulcrum distance L, a positioning hole 13 is processed on a frame type cross beam 12, the elastic support 1 assembly is integrally fixed and inserted into the corresponding positioning hole 13, an elastic support hook plate 8 is fixed on the side surface of the elastic support 1, a hasp handle 11 is pulled off, a hasp ring nut 20 is adjusted to a proper length and is buckled on the hook plate 8, the hasp handle 11 is pushed upwards until the front surface and the rear surface of the elastic support are close to each other, and a quick-release spring pin 3 is inserted into a hasp base 18, so that the hasp handle 11 is prevented from falling off due to stress. Bolts at the bottom of the spring seat adapter plate 19 penetrate through the frame-type beam 12 and are fastened at the bottom by self-locking nuts or double nuts.

Place the projectile body 2 on the 1 subassembly of a, b two places bullet support, and the fulcrum position needs to be unanimous with the 1 fulcrum position of projectile body, because projectile body 2 directly places and can have the rotation on the 1 subassembly of bullet support, need twine sack 5 on the surface of projectile body 2, pull out quick-release spring catch 3, adjust hasp ring nut 20, make it closely detain mutually with couple board 8, promote hasp handle 11 downwards, make couple board 8 closely detain mutually with hasp ring nut 20, let antistatic rubber 10 on the sack 5 and 2 surface contact of projectile body, increase frictional force, insert quick-release spring catch 3, prevent the rotation of projectile body.

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.