CN219454852U

CN219454852U - Body dismounting device of air-ground missile

Info

Publication number: CN219454852U
Application number: CN202223577932.1U
Authority: CN
Inventors: 杨晓东; 陈明明; 龙涛
Original assignee: Rainbow UAV Technology Co Ltd
Current assignee: Rainbow UAV Technology Co Ltd
Priority date: 2022-12-30
Filing date: 2022-12-30
Publication date: 2023-08-01
Anticipated expiration: 2032-12-30

Abstract

The utility model provides a body disassembling device of an air-to-ground missile, which relates to the technical field of missile disassembly, and comprises the following components: the two clamping assemblies comprise two clamping parts, one sides of the two clamping parts, which are close to each other, are provided with clamping grooves, the two clamping parts can clamp the body of the air-to-ground missile through the respective clamping grooves, the two clamping parts are connected through connecting bolts, and the distance between the two clamping parts can be adjusted through the connecting bolts; the middle part of the top loosening bolt is in threaded connection in one of the clamping assemblies, one end of the top loosening bolt is used for propping against the other clamping assembly, and the distance between the two clamping assemblies can be adjusted through the top loosening bolt; the problem that the cabin sections of the body of the air-to-ground missile are difficult to detach due to the requirement of tightness is solved.

Description

Body dismounting device of air-ground missile

Technical Field

The utility model belongs to the technical field of missile disassembly, and particularly relates to a missile body disassembly device of an air-to-ground missile.

Background

In the development and production process of the air-to-ground missile, in order to avoid corrosion damage of equipment and metal parts in the missile, the air-to-ground missile can provide a sealing requirement, in the butt joint process of the cabin sections of the body of the air-to-ground missile, a butt joint surface of the body of the missile is generally sealed by using sealant, a sealing effect is achieved after the colloid is dried, and meanwhile, difficulty is caused in disassembling the cabin sections of the body of the missile.

After the air-to-ground missile experiment shell is launched, in order to acquire relevant experiment data, relevant equipment in the missile needs to be taken out for data analysis. Because the air-to-ground missile generates larger impact when striking the ground, the missile body can be greatly deformed, and therefore, the disassembly between cabin sections of the missile body can be difficult.

Disclosure of Invention

The utility model aims to provide a body disassembling device for an air-to-ground missile, which solves the problem that the cabin sections of the body of the air-to-ground missile are difficult to disassemble due to the requirement of tightness.

In order to achieve the above object, the present utility model provides a body detaching device for an air-to-ground missile, including:

the two clamping assemblies comprise two clamping parts, one sides of the two clamping parts, which are close to each other, are provided with clamping grooves, the two clamping parts can clamp the body of the air-ground missile through the respective clamping grooves, the two clamping parts are connected through connecting bolts, and the distance between the two clamping parts can be adjusted through the connecting bolts;

the middle part threaded connection of top pine bolt is in one of them the centre gripping subassembly, the one end of top pine bolt is used for with another wherein the centre gripping subassembly is supported and is leaned on, through top pine bolt can adjust two distance between the centre gripping subassembly.

Optionally, each clamping part comprises an arc-shaped part and connecting lugs which are arranged on two sides of the arc-shaped part and extend outwards, and connecting holes are formed in the connecting lugs.

Optionally, the connecting bolt is movably arranged in the connecting hole in a penetrating way, and the connecting bolt is connected with an adjusting nut in a threaded way.

Optionally, gaskets are arranged between the nuts of the adjusting bolts and the connecting lugs and between the adjusting nuts and the connecting lugs.

Optionally, a rubber pad is arranged on the groove wall of the clamping groove.

Optionally, grooves are provided at the bottoms of the two clamping grooves of each clamping assembly.

Optionally, the loose top bolts are provided in two, and the loose top bolts are respectively provided at two sides of one of the clamping assemblies.

Optionally, two sides of one clamping part of one clamping assembly are respectively provided with a threaded hole, and two loose top bolts are respectively in threaded connection with the two threaded holes.

Optionally, the material of the clamping part is aluminum alloy.

Optionally, the clamping grooves of the two clamping assemblies are respectively matched with the shapes of the bodies of the air-ground missiles at different positions.

The utility model provides a body dismounting device for an air-to-ground missile, which has the beneficial effects that: the device has two clamping components, two clamping components can be through the regulation of respective connecting bolt, the different positions of the hull of air-ground missile are lived respectively, make the seam between two cabin sections of hull be in between two clamping components, then utilize the loose top bolt to adjust the distance between two clamping components, utilize the one end of loose top bolt and clamping component's effect of supporting, make two clamping components and two cabin sections separation, and then realize the convenient dismantlement of hull of air-ground missile, in this dismantlement process, the manpower can be with the hull light disassemble, and labour saving and time saving during the use, and the device simple structure, portable, convenient operation, can alleviate the production of air-ground missile and the production personnel in the experiment and the laboratory personnel's work load greatly.

Additional features and advantages of the utility model will be set forth in the detailed description which follows.

Drawings

The foregoing and other objects, features and advantages of the utility model will be apparent from the following more particular descriptions of exemplary embodiments of the utility model as illustrated in the accompanying drawings wherein like reference numbers generally represent like parts throughout the exemplary embodiments of the utility model.

FIG. 1 shows a schematic front view of a projectile removal device for an air-to-ground projectile in accordance with one embodiment of the utility model.

FIG. 2 illustrates a schematic side view of a projectile removal device for an air-to-ground projectile in accordance with one embodiment of the utility model.

Reference numerals illustrate:

1. a clamping part; 2. a clamping groove; 3. a connecting bolt; 4. loosening the bolt; 5. a connecting lug; 6. an adjusting nut; 7. a gasket; 8. and a rubber pad.

Detailed Description

Preferred embodiments of the present utility model will be described in more detail below. While the preferred embodiments of the present utility model are described below, it should be understood that the present utility model may be embodied in various forms and should not be limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the utility model to those skilled in the art.

As shown in fig. 1 and 2, the present utility model provides a body detaching device for an air-to-ground missile, including:

the two clamping assemblies, each clamping assembly comprises two clamping parts 1, a clamping groove 2 is formed in one side, close to each other, of each clamping part 1, the two clamping parts 1 can clamp the body of the air-ground missile through the corresponding clamping groove 2, the two clamping parts 1 are connected through a connecting bolt 3, and the distance between the two clamping parts 1 can be adjusted through the connecting bolt 3;

the top loose bolt 4, the middle part threaded connection of top loose bolt 4 is in one of them clamping assembly, and the one end of top loose bolt 4 is used for with wherein another clamping assembly supports, can adjust the distance between two clamping assembly through top loose bolt 4.

Specifically, in order to solve the problem that the hull of the air-to-ground missile is difficult to disassemble due to the requirement of tightness, the hull disassembly device of the air-to-ground missile provided by the utility model is provided with two clamping assemblies, the two clamping assemblies can respectively clamp different positions of the hull of the air-to-ground missile through the adjustment of respective connecting bolts 3, so that a seam between the two hull sections of the hull is positioned between the two clamping assemblies, then the distance between the two clamping assemblies is adjusted by using a top loose bolt 4, and the two clamping assemblies are separated from the two hull sections by using the abutting action of one end of the top loose bolt 4, so that the hull of the air-to-ground missile can be disassembled easily by manpower in the disassembly process.

Optionally, each clamping part 1 comprises an arc-shaped part and connecting lugs 5 which are arranged on two sides of the arc-shaped part and extend outwards, and connecting holes are formed in the connecting lugs 5.

Specifically, the arc-shaped part can be a strip-shaped part bent into an arc shape, so that the arc-shaped part has enough hardness and strength, one side of the arc-shaped part is provided with a concave clamping groove 2, and two clamping grooves 2 of each clamping assembly are mutually close to and communicated and are used for clamping a bullet body; the connecting lug 5 and the arc-shaped part are integrally formed and extend outwards, so that the adjusting operation of the connecting bolt 3 is facilitated.

Optionally, the connecting bolt 3 is movably arranged in the connecting hole in a penetrating way, and the adjusting nut 6 is connected to the connecting bolt 3 in a threaded way.

Specifically, the nuts of the connecting bolts 3 and the adjusting nuts 6 are respectively positioned at two outer sides of the two clamping parts 1 of the same clamping assembly, and the two clamping parts 1 can be mutually close to each other to clamp the body of the bullet by screwing the adjusting nuts 6.

Optionally, shims 7 are provided between the nut of the adjusting bolt and the connecting lug 5 and between the adjusting nut 6 and the connecting lug 5.

Specifically, the arrangement of the gasket 7 prevents the nut of the adjusting bolt and the adjusting nut 6 from directly contacting with the connecting lug 5, so that the connecting lug 5 is damaged, and the service life of the device is prolonged.

Optionally, a rubber pad 8 is provided on the groove wall of the clamping groove 2.

Specifically, the rubber pad 8 is arranged to avoid the clamping part 1 from scratching the body of a bullet.

Optionally, the bottoms of the two clamping grooves 2 of each clamping assembly are provided with grooves.

Specifically, the arrangement of the groove can avoid the structure of the outside evagination such as the ventral fin and the socket on the bullet body.

Alternatively, two top loosening bolts 4 are provided, and two top loosening bolts 4 are respectively provided at both sides of one of the clamping assemblies.

Specifically, two loose top bolts 4 are arranged, so that the other clamping assembly can be jacked from the two sides of one clamping assembly, and the disassembly efficiency is improved.

Optionally, two sides of a clamping part 1 of one of the clamping assemblies are respectively provided with a threaded hole, and two loose top bolts 4 are respectively in threaded connection with the two threaded holes.

Specifically, when the top loosening bolt 4 is turned, one end of the top loosening bolt 4 abuts against the other clamping component, and the other clamping component is pushed outwards.

Optionally, the material of the clamping portion 1 is an aluminum alloy.

Specifically, the clamping part 1 made of aluminum alloy material has light weight and is convenient to operate and move.

Alternatively, the clamping grooves 2 of the two clamping assemblies are respectively matched with the shapes of the bodies of the air-to-ground missiles at different positions.

Specifically, the shape and the size of the respective clamping groove 2 of the two clamping assemblies can be set according to the actual disassembly position of the body of the bullet, so that the body cabin sections at different positions of the air-to-ground missile can be conveniently disassembled.

The foregoing description of embodiments of the utility model has been presented for purposes of illustration and description, and is not intended to be exhaustive or limited to the embodiments disclosed. Many modifications and variations will be apparent to those of ordinary skill in the art without departing from the scope and spirit of the various embodiments described.

Claims

1. A body detaching device for an air-to-ground missile, the device comprising:

2. The air-to-ground missile body removing device according to claim 1, wherein each clamping portion comprises an arc portion and connecting lugs which are arranged on two sides of the arc portion and extend outwards, and connecting holes are formed in the connecting lugs.

3. The body removing device for an air-to-ground missile according to claim 2, wherein the connecting bolt is movably inserted into the connecting hole, and an adjusting nut is connected to the connecting bolt through threads.

4. A body disassembly device for an air-to-ground missile according to claim 3, wherein gaskets are provided between the nut of the connecting bolt and the connecting lug and between the adjusting nut and the connecting lug.

5. The air-to-ground missile body dismounting device according to claim 1, wherein a rubber pad is arranged on a groove wall of the clamping groove.

6. The air-to-ground missile body removing device according to claim 1, wherein grooves are formed in bottoms of two clamping grooves of each clamping assembly.

7. The air-to-ground missile body dismounting device of claim 1, wherein two top loose bolts are provided, and two top loose bolts are respectively provided at both sides of one of the clamping assemblies.

8. The air-to-ground missile body dismounting device according to claim 7, wherein two sides of one clamping portion of one clamping assembly are respectively provided with a threaded hole, and two top loose bolts are respectively in threaded connection with two threaded holes.

9. The air-to-ground missile body removing device according to claim 1, wherein the material of the clamping portion is aluminum alloy.

10. The hull disassembly device of an air-to-ground missile according to claim 1, wherein the clamping grooves of the two clamping assemblies are respectively matched with the shapes of the hulls at different positions of the air-to-ground missile.