CN214722367U

CN214722367U - Fixture for missile parts

Info

Publication number: CN214722367U
Application number: CN202120283196.5U
Authority: CN
Inventors: 郑战奎; 柳晨静
Original assignee: Hebei Huaye Machinery Technology Co ltd
Current assignee: Hebei Huaye Machinery Technology Co ltd
Priority date: 2021-02-01
Filing date: 2021-02-01
Publication date: 2021-11-16
Anticipated expiration: 2031-02-01

Abstract

The utility model discloses a guided missile spare part anchor clamps, the load simulator comprises a case, clamping mechanism and side shield device that the longitudinal symmetry set up, side shield device sets up in clamping mechanism's lower extreme, clamping mechanism all sets up in the inside of quick-witted case with side shield device, the right-hand member of machine case is provided with the cushion collar, the front end is provided with the pivot, clamping mechanism is including pressing from both sides the groove, compression spring, first briquetting and centre gripping cavity, the centre gripping cavity sets up in the right-hand member of first briquetting, first briquetting sets up in compression spring's right-hand member, compression spring, first briquetting and centre gripping cavity all set up in the inside of pressing from both sides the groove, be provided with the sliding block on the inner wall of pressing from both sides the groove, be provided with the chute on the inner wall of sliding block, the lower extreme of chute is provided with the second briquetting, the lower extreme of second briquetting is worn to locate on the centre gripping cavity, the inside of centre gripping cavity is provided with the guided missile part. The utility model adopts the above device a guided missile spare part anchor clamps has sufficient clamp force, simple structure, and work efficiency is high.

Description

Fixture for missile parts

Technical Field

The utility model belongs to the technical field of fixture equipment technique and specifically relates to a guided missile spare part anchor clamps are related to.

Background

The missile becomes the first choice ammunition for realizing accurate strike in modern war due to the characteristics of strong killing power, small collateral damage, short reaction time, high combat efficiency, accurate strike and the like, the existing clamping of the missile rudder piece on a machine tool is a difficult process, and the clamping device only clamps the missile rudder piece left and right and does not clamp the missile rudder piece up and down, so that the clamping force of the missile rudder piece is insufficient, and the working efficiency is influenced.

SUMMERY OF THE UTILITY MODEL

The utility model aims at providing a guided missile spare part anchor clamps has sufficient clamp force, simple structure, and work efficiency is high.

In order to achieve the purpose, the utility model provides a missile part clamp, which comprises a case, a clamping mechanism and a side baffle device, wherein the clamping mechanism and the side baffle device are arranged in an up-down symmetrical manner;

clamping mechanism is including pressing from both sides groove, compression spring, first briquetting and centre gripping cavity, the centre gripping cavity set up in the right-hand member of first briquetting, first briquetting set up in compression spring's right-hand member, compression spring first briquetting with the centre gripping cavity all set up in press from both sides the inside in groove, be provided with the sliding block on the inner wall in clamp groove, be provided with the chute on the inner wall of sliding block, the lower extreme of chute is provided with the second briquetting, the lower extreme of second briquetting is worn to locate on the centre gripping cavity, the inside of centre gripping cavity is provided with the guided missile part.

Preferably, the lower end of the second pressing block is provided with a convex block, the lower end of the convex block abuts against the missile component, a rubber sleeve is arranged on the convex block, and the second pressing block is in sliding connection with the chute.

Preferably, the chute gradually increases from right to left.

Preferably, the side baffle device comprises an electric slide rail arranged inside the case, an installation box arranged at the upper end of the electric slide rail, an air cylinder arranged inside the installation box and a stop block arranged at the upper end of the air cylinder, and the upper end of the stop block penetrates through the case.

Preferably, be provided with the guide bar on the clamp groove, the guide bar wears to locate the sliding block is last, the sliding block with the inner wall in clamp groove is sliding connection.

Therefore, the utility model adopts the above device a guided missile spare part anchor clamps has sufficient clamp force, simple structure, and work efficiency is high.

The technical solution of the present invention is further described in detail by the accompanying drawings and examples.

Drawings

FIG. 1 is a schematic structural view of an embodiment of a missile component fixture of the present invention;

FIG. 2 is a schematic view of a clamping mechanism of an embodiment of a missile component fixture of the present invention;

1, a case; 2. a clamping mechanism; 3. a buffer table; 4. a rotating shaft; 5. a clamping groove; 6. a compression spring; 7. a first pressing block; 8. a clamping cavity; 9. a slider; 10. a chute; 11. a second pressing block; 12. a bump; 13. a guide bar; 14. an electric slide rail; 15. installing a box; 16. a cylinder; 17. and a stop block.

Detailed Description

The technical solution of the present invention is further explained by the accompanying drawings and examples.

Unless defined otherwise, technical or scientific terms used herein shall have the ordinary meaning as understood by those of ordinary skill in the art to which the invention belongs. The use of "first," "second," and similar terms in the description herein do not denote any order, quantity, or importance, but rather the terms are used to distinguish one element from another. The word "comprising" or "comprises", and the like, means that the element or item listed before the word covers the element or item listed after the word and its equivalents, but does not exclude other elements or items. The terms "connected" or "coupled" and the like are not restricted to physical or mechanical connections, but may include electrical connections, whether direct or indirect. "upper", "lower", "left", "right", and the like are used merely to indicate relative positional relationships, and when the absolute position of the object being described is changed, the relative positional relationships may also be changed accordingly.

Examples

Referring to fig. 1 and 2, the utility model provides a guided missile spare part anchor clamps, including quick-witted case 1, the clamping mechanism 2 and the side shield device that the longitudinal symmetry set up, the side shield device sets up in clamping mechanism 2's lower extreme, and clamping mechanism 2 all sets up in quick-witted case 1's inside with the side shield device, and the right-hand member of quick-witted case 1 is provided with cushion table 3, makes things convenient for the guided missile part to take out and places, and the front end is provided with pivot 4, and pivot 4 is fixed through the chuck and is worked on the lathe.

Clamping mechanism 2 is including pressing from both sides groove 5, compression spring 6, first briquetting 7 and centre gripping cavity 8, centre gripping cavity 8 sets up in the right-hand member of first briquetting 7, first briquetting 7 sets up in compression spring 6's right-hand member, compression spring 6, first briquetting 7 and centre gripping cavity 8 all set up in the inside of pressing from both sides groove 5, be provided with sliding block 9 on the inner wall of clamp groove 5, be provided with chute 10 on sliding block 9's the inner wall, chute 10's lower extreme is provided with second briquetting 11, the lower extreme of second briquetting 11 is worn to locate on centre gripping cavity 8, the inside of centre gripping cavity 8 is provided with the guided missile part. The lower end of the second pressing block 11 is provided with a convex block 12, the lower end of the convex block 12 is abutted to the missile component, a rubber sleeve is arranged on the convex block 12 to prevent the convex block 12 and the missile component from being worn, the second pressing block 11 is in sliding connection with the chute 10, and the structure plays a role in fixing the upper end and the lower end of the missile component. The chute 10 is gradually increased from right to left, and when the missile component moves rightwards, the chute 10 can gradually reduce the pressing force on the lug 12, so that the pressing force of the lug 12 on the missile component is gradually reduced, and the missile component is stably moved out. Be provided with guide bar 13 on the clamp groove 5, guide bar 13 wears to locate on sliding block 9, and sliding block 9 is sliding connection with the inner wall that presss from both sides groove 5, and sliding block 9 slides on pressing from both sides groove 5 and through guide bar 13's guide effect, makes its gliding more stable.

The side baffle device comprises an electric slide rail 14 arranged inside the case 1, an installation box 15 arranged at the upper end of the electric slide rail 14, an air cylinder 16 arranged inside the installation box 15 and a stop block 17 arranged at the upper end of the air cylinder 16, wherein the upper end of the stop block 17 penetrates through the case 1. When the missile starting device works, the air cylinder 16 is started, the air cylinder 16 drives the stop block 17 to ascend, and meanwhile, the electric sliding rail 14 is started, so that the stop block 17 moves leftwards and abuts against the right end of the missile part, and the left end of the missile part is pressed on the first pressing block 7.

When the device works for clamping the missile part, the missile part is firstly loaded into the clamping cavity 8, the air cylinder 16 is started, the air cylinder 16 drives the stop block 17 to ascend, and meanwhile, the electric slide rail 14 is started, so that the stop block 17 moves leftwards to abut against the right end of the missile part, the left end of the missile part is pressed on the first press block 7, and meanwhile, the upper end and the lower end of the missile part abut against the convex block 12 to be clamped. When the missile part needs to be taken out, the air cylinder 16 is started to enable the stop block 17 to retract into the installation box 15, the installation box 15 is moved back to the original position through the electric slide rail 14, meanwhile, the right pressing force of the missile part is lost, the missile part is pushed to the right end through the compression spring 6, the lug 12 at the upper end moves rightwards to leave the missile device, the upper end and the lower end of the missile device lose the pressing force, and finally, the missile part is taken out.

Finally, it should be noted that: the above embodiments are only for illustrating the technical solutions of the present invention and not for limiting the same, and although the present invention is described in detail with reference to the preferred embodiments, those skilled in the art should understand that: the technical solution of the present invention can still be modified or replaced by other equivalent means, and the modified technical solution can not be separated from the spirit and scope of the technical solution of the present invention.

Claims

1. A missile part anchor clamps which characterized in that:

the clamping mechanism and the side baffle device are both arranged in the case, the right end of the case is provided with a buffer table, and the front end of the case is provided with a rotating shaft;

2. The missile component fixture of claim 1, wherein: the lower end of the second pressing block is provided with a convex block, the lower end of the convex block is abutted to the missile component, a rubber sleeve is arranged on the convex block, and the second pressing block is in sliding connection with the chute.

3. The missile component fixture of claim 2, wherein: the chute gradually increases from right to left.

4. The missile component fixture of claim 1, wherein: the side baffle device comprises an electric slide rail arranged in the case, an installation box arranged at the upper end of the electric slide rail, an air cylinder arranged in the installation box and a stop block arranged at the upper end of the air cylinder, wherein the upper end of the stop block penetrates through the case.

5. The missile component fixture of claim 1, wherein: be provided with the guide bar on the clamp groove, the guide bar wears to locate the last of sliding block, the sliding block with the inner wall that presss from both sides the groove is sliding connection.