CN220197402U - Missile casing processing location frock - Google Patents

Abstract

The utility model discloses a missile shell processing and positioning tool which comprises a positioning tool body, a chassis and a limiting box, wherein a second electric push rod is fixedly connected inside the limiting box, the output end of the second electric push rod is fixedly connected with a first fixed arc plate, the outer wall of the first fixed arc plate is fixedly connected with a connecting plate, the connecting plates are fixedly connected through bolts, the outer wall of the connecting plate is fixedly connected with a second fixed arc plate, mounting grooves are respectively and fixedly connected between the first fixed arc plate and the second fixed arc plate, a push rod is slidably connected inside the mounting grooves, the outer wall of the push rod is rotatably connected with a rotating shaft, and the outer wall of the rotating shaft is fixedly connected with a clamping plate. This guided missile casing processing location frock promotes the restriction case and slides along the spout inside through starting electric putter along the restriction piece, is convenient for adjust the distance between two first fixed arc boards and the fixed arc boards of two second, and is convenient for according to the casing size adjustment position of guided missile casing processing.

Description

Missile casing processing location frock

Technical Field

The utility model belongs to the technical field of missile shell machining, and particularly relates to a missile shell machining positioning tool.

Background

The missile shell is a main body for manufacturing the missile, and when the missile shell is processed, in order to facilitate the operation of staff, the missile shell needs to be positioned and locked by utilizing a positioning tool, so that the phenomenon that the missile shell is offset due to the driving force of processing equipment is avoided.

Because the missile shell has the size difference, the positioning tool is difficult to adapt to the missile shells with different sizes to clamp and fix, the flexibility of operation is lower, the missile shells cannot be positioned on the same horizontal line independently when being positioned and locked, the position of the missile shells is inclined, and when the missile shells are processed, the measurement and assembly between parts cannot be accurately carried out.

Disclosure of Invention

The utility model aims to provide a missile shell machining and positioning tool for solving the technical problems in the background technology.

In order to achieve the above purpose, the specific technical scheme of the utility model is as follows: the utility model provides a guided missile casing processing location frock, includes location frock body, quick-witted case and restriction case, the inside fixedly connected with second electric putter of restriction case, the first fixed arc board of second electric putter output fixedly connected with, first fixed arc board outer wall fixedly connected with connecting plate, through bolt fixed connection between the connecting plate, the fixed arc board of connecting plate outer wall fixedly connected with second, respectively fixedly connected with mounting groove between first fixed arc board and the fixed arc board of second, the inside sliding connection of mounting groove has the push rod, the push rod outer wall rotates and is connected with the pivot, pivot outer wall fixedly connected with grip block.

Preferably, the two sides of the outer wall of the positioning tool body are respectively and fixedly connected with a case, the inside of the case is fixedly connected with a first electric push rod, and the output end of the first electric push rod is fixedly connected with a limiting case.

Preferably, a spring is fixedly connected in the mounting groove, and one end of the spring is fixedly connected with the push rod.

Preferably, the inside front and back both sides of location frock body have seted up the spout respectively, the inside sliding connection of spout has the restriction piece, restriction piece outer wall fixedly connected with restriction case.

Preferably, the number of the clamping plates is four, and the four clamping plates are symmetrically arranged by taking connecting lines between the connecting plates as centers.

Preferably, the first fixed arc plate and the second fixed arc plate are symmetrically arranged.

The missile shell machining and positioning tool has the following advantages:

1. this guided missile casing processing location frock promotes restriction case and slides along the spout inside along the restriction piece through starting electric putter, is convenient for adjust the distance between two first fixed arc plates and two second fixed arc plates, and is convenient for according to the casing size adjustment position of guided missile casing processing, and promotes first fixed arc plate and the fixed arc plate height-adjusting of second through starting second electric putter, is convenient for according to the position adjustment height of the casing size of guided missile casing processing.

2. Through being provided with the spring inside the mounting groove, the elastic adjustment through the spring is to the big pressure of the casing size of guided missile casing processing, and through being provided with the rotation between grip block and the push rod and be connected, the rotation angle of grip block is convenient for adjust according to the shape of casing.

Drawings

In order to more clearly illustrate the technical solutions of the embodiments of the present utility model, the drawings that are needed in the embodiments will be briefly described below, it being understood that the following drawings only illustrate some examples of the present utility model and therefore should not be considered as limiting the scope, and other related drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.

FIG. 1 is a schematic diagram of the overall internal structure of the present utility model;

FIG. 2 is a schematic top view of the present utility model

FIG. 3 is a schematic side view of the present utility model;

FIG. 4 is an enlarged schematic view of the structure of FIG. 1A according to the present utility model;

the figure indicates: 1. positioning the tool body; 2. a chassis; 3. a first electric push rod; 4. a chute; 5. a limiting block; 6. a limit box; 7. a second electric push rod; 8. a first fixed arc plate; 9. a connecting plate; 10. a second fixed arc plate; 11. a clamping plate; 12. a limiting groove; 13. a mounting groove; 14. a spring; 15. a push rod; 16. a rotating shaft.

Detailed Description

Hereinafter, only certain exemplary embodiments are briefly described. As will be recognized by those of skill in the pertinent art, the described embodiments may be modified in numerous different ways without departing from the spirit or scope of the embodiments of the present utility model. Accordingly, the drawings and description are to be regarded as illustrative in nature and not as restrictive.

In the description of the embodiments of the present utility model, it should be understood that the terms "length," "vertical," "horizontal," "top," "bottom," and the like indicate an orientation or a positional relationship based on that shown in the drawings, and are merely for convenience in describing the embodiments of the present utility model and to simplify the description, rather than to indicate or imply that the devices or elements referred to must have a specific orientation, be configured and operated in a specific orientation, and thus should not be construed as limiting the embodiments of the present utility model.

Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying a relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defining "a first" or "a second" may explicitly or implicitly include one or more such feature. In the description of the embodiments of the present utility model, the meaning of "plurality" is two or more, unless explicitly defined otherwise.

In the embodiments of the present utility model, unless explicitly specified and limited otherwise, the terms "mounted," "connected," "secured" and the like are to be construed broadly and include, for example, either permanently connected, removably connected, or integrally formed; the device can be mechanically connected, electrically connected and communicated; can be directly connected or indirectly connected through an intermediate medium, and can be communicated with the inside of two elements or the interaction relationship of the two elements. The specific meaning of the above terms in the embodiments of the present utility model will be understood by those of ordinary skill in the art according to specific circumstances.

The following disclosure provides many different implementations, or examples, for implementing different configurations of embodiments of the utility model. In order to simplify the disclosure of embodiments of the present utility model, components and arrangements of specific examples are described below. Of course, they are merely examples and are not intended to limit embodiments of the present utility model. Furthermore, embodiments of the present utility model may repeat reference numerals and/or letters in the various examples, which are for the purpose of brevity and clarity, and which do not themselves indicate the relationship between the various embodiments and/or arrangements discussed.

In order to better understand the purpose, structure and function of the utility model, a missile shell processing and positioning tool of the utility model is described in further detail below with reference to the accompanying drawings.

As shown in fig. 1-4, the missile shell processing and positioning tool comprises a positioning tool body 1, a case 2 and a limiting box 6, wherein a second electric push rod 157 is fixedly connected inside the limiting box 6, the output end of the second electric push rod 157 is fixedly connected with a first fixed arc plate 8, the outer wall of the first fixed arc plate 8 is fixedly connected with a connecting plate 9, the connecting plates 9 are fixedly connected through bolts, the outer walls of the connecting plates 9 are fixedly connected with a second fixed arc plate 10, mounting grooves 13 are respectively and fixedly connected between the first fixed arc plate 8 and the second fixed arc plate 10, push rods 15 are slidably connected inside the mounting grooves 13, a rotating shaft 16 is rotatably connected to the outer walls of the push rods 15, clamping plates 11 are fixedly connected to the outer walls of the rotating shaft 16, two sides of the outer walls of the positioning tool body 1 are respectively and fixedly connected with the case 2, the inner sides of the case 2 are fixedly connected with first electric push rods 153, the output end of the first electric push rods 153 is fixedly connected with the limiting box 6, springs 14 are fixedly connected inside the mounting grooves 13, one ends of the springs 14 are fixedly connected with the push rods 15, sliding grooves 4 are respectively arranged on the front side and rear side of the inner sides of the positioning tool body 1, limiting blocks 5 are slidably connected with limiting blocks 5, the outer walls of the limiting blocks 5 are fixedly connected with the four connecting plates 11, and the four clamping plates 11 are arranged symmetrically, and are arranged as the four symmetrical clamping plates and are arranged as the two center plates 8 and are fixedly and are arranged as the center plates 11.

Working principle: the limiting box 6 is pushed by the electric push rod 15 to slide along the inside of the sliding groove 4 along the limiting block 5, the distance between the two first fixed arc plates 8 and the two second fixed arc plates 10 is convenient to adjust, the position is convenient to adjust according to the shell size of the missile shell processing, the height is convenient to adjust according to the position of the shell size of the missile shell processing by pushing the first fixed arc plates 8 and the second fixed arc plates 10 by the electric push rod 157, the spring 14 is arranged inside the mounting groove 13, the pressure on the shell size of the missile shell processing is adjusted through the elasticity of the spring 14, and the rotation connection is arranged between the clamping plate 11 and the push rod 15, so that the rotation angle of the clamping plate 11 is convenient to adjust according to the shape of the shell.

It will be understood that the utility model has been described in terms of several embodiments, and that various changes and equivalents may be made to these features and embodiments by those skilled in the art without departing from the spirit and scope of the utility model. In addition, many modifications may be made to adapt a particular situation or material to the teachings of the utility model without departing from the essential scope thereof. Therefore, it is intended that the utility model not be limited to the particular embodiment disclosed, but that the utility model will include all embodiments falling within the scope of the appended claims.

Claims (6)

1. The utility model provides a guided missile casing processing location frock, includes location frock body (1), quick-witted case (2) and restriction case (6), its characterized in that: the limiting box is characterized in that a second electric push rod (7) is fixedly connected to the inside of the limiting box (6), a first fixed arc plate (8) is fixedly connected to the output end of the second electric push rod (7), a connecting plate (9) is fixedly connected to the outer wall of the first fixed arc plate (8), the connecting plates (9) are fixedly connected through bolts, a second fixed arc plate (10) is fixedly connected to the outer wall of the connecting plate (9), a mounting groove (13) is respectively and fixedly connected between the first fixed arc plate (8) and the second fixed arc plate (10), a push rod (15) is connected to the inside of the mounting groove (13) in a sliding mode, a rotating shaft (16) is connected to the outer wall of the push rod (15) in a rotating mode, and a clamping plate (11) is fixedly connected to the outer wall of the rotating shaft (16).

2. The missile hull machining positioning tool of claim 1, wherein: the positioning tool comprises a positioning tool body (1), wherein two sides of the outer wall of the positioning tool body are fixedly connected with a machine case (2) respectively, a first electric push rod (3) is fixedly connected inside the machine case (2), and the output end of the first electric push rod (3) is fixedly connected with a limiting case (6).

3. The missile hull machining positioning tool of claim 1, wherein: the spring (14) is fixedly connected inside the mounting groove (13), and one end of the spring (14) is fixedly connected with the push rod (15).

4. The missile hull machining positioning tool of claim 1, wherein: the positioning tool comprises a positioning tool body (1), wherein sliding grooves (4) are respectively formed in the front side and the rear side of the inner portion of the positioning tool body, limiting blocks (5) are connected inside the sliding grooves (4) in a sliding mode, and limiting boxes (6) are fixedly connected to the outer walls of the limiting blocks (5).

5. The missile hull machining positioning tool of claim 1, wherein: the number of the clamping plates (11) is four, and the four clamping plates (11) are symmetrically arranged by taking connecting lines between the connecting plates (9) as centers.

6. The missile hull machining positioning tool of claim 1, wherein: the first fixed arc plate (8) and the second fixed arc plate (10) are symmetrically arranged.