CN209246818U - A kind of guided missile Zhen Ci housing into rotation mechanism - Google Patents
A kind of guided missile Zhen Ci housing into rotation mechanism Download PDFInfo
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- CN209246818U CN209246818U CN201821810989.2U CN201821810989U CN209246818U CN 209246818 U CN209246818 U CN 209246818U CN 201821810989 U CN201821810989 U CN 201821810989U CN 209246818 U CN209246818 U CN 209246818U
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- plug
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- guided missile
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- housing
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Abstract
The utility model discloses a kind of guided missile Zhen Ci housing into rotation mechanisms, it include: body, taper die, plug, plug pedestal, cone rotating electric machine and cone oscillating motor, plug pedestal is provided on the body, described plug one end is arranged with taper die, the plug other end is connect with plug pedestal, cone rotating electric machine and cone oscillating motor are provided on the body, the cone rotating electric machine is connect with plug base drive, the plug bottom end is arranged with plug set, the cone oscillating motor and plug set are sequentially connected, missile case is provided on the taper die.By the above-mentioned means, guided missile Zhen Ci housing into rotation mechanism provided by the utility model, substitution is artificial, and when needle pierces processing carbon fiber, straight forming guided missile body, fiber fleece uniformity is good, can satisfy the production requirement of guided missile quality.
Description
Technical field
The utility model relates to needing machine tool apparatus fields, more particularly to a kind of guided missile Zhen Ci housing into rotation mechanism.
Background technique
In order to improve the carrying capacity of guided missile, body structure quality should mitigate as far as possible.Therefore the material of high specific strength should be used
Material and advanced structure type, guided missile shape are to influence one of the principal element of missile performance, it is necessary to have good pneumatic outer
Shape is in conical form structure.Carbon fiber is the material of high-strength specific strength, applied on space flight, guided missile, can significantly mitigate weight
Amount improves payload, improves performance.Currently, processing carbon fiber guided missile product cannot use mechanical equipment because of contour structures
Processing, is controlled by manual operation, is manually successively coated with carbon fiber stratum reticulare, manually pierces winding processing in guided missile mold needle, raw
Low efficiency is produced, needling density is uneven, cannot achieve volume production production.It is processed into blocky carbon fibre fabric by plate needing machine,
The compound processed center turning of carbon carbon forms guided missile, generates a large amount of waste leftover material, and turnery processing size not can guarantee, also without
Method realizes volume production production.
Summary of the invention
For the utility model mainly solving the technical problems that providing a kind of guided missile Zhen Ci housing into rotation mechanism, substitution is artificial,
When needle pierces processing carbon fiber, straight forming guided missile body, fiber fleece uniformity is good, and the production that can satisfy guided missile quality is wanted
It asks.
In order to solve the above technical problems, the technical solution that the utility model uses is: providing a kind of guided missile needle thorn shell
Body rotating mechanism, comprising: body, taper die, plug, plug pedestal, cone rotating electric machine and cone oscillating motor, the machine
Plug pedestal is provided on body, described plug one end is arranged with taper die, and the plug other end is connect with plug pedestal, institute
It states and is provided with cone rotating electric machine and cone oscillating motor on body, the cone rotating electric machine is connect with plug base drive,
The plug bottom end is arranged with plug set, and the cone oscillating motor and plug set are sequentially connected, are arranged on the taper die
There is missile case.
In one preferred embodiment of the utility model, the taper die can carry out 360 degree rotation.
In one preferred embodiment of the utility model, the taper die can carry out 180 swings.
In one preferred embodiment of the utility model, the cone rotating electric machine and cone oscillating motor with stepping control
System connection processed.
In one preferred embodiment of the utility model, the body side is provided with cone support base, the cone branch
Supportting seat includes support screw and support plate, and the support plate is connected with the top of support screw by shaft.
The beneficial effects of the utility model are: a kind of guided missile Zhen Ci housing into rotation mechanism that the utility model is pointed out, substitution
Manually, when needle pierces processing carbon fiber, straight forming guided missile body, fiber fleece uniformity is good, can satisfy guided missile quality
Production requirement.
Detailed description of the invention
It, below will be to required in embodiment description in order to illustrate more clearly of the technical scheme in the embodiment of the utility model
Attached drawing to be used is briefly described, it should be apparent that, the accompanying drawings in the following description is only some realities of the utility model
Example is applied, it for those of ordinary skill in the art, without creative efforts, can also be according to these attached drawings
Obtain other attached drawings, in which:
Fig. 1 is a kind of structural schematic diagram of one preferred embodiment of guided missile Zhen Ci housing into rotation mechanism of the utility model.
Specific embodiment
Below by the technical scheme in the utility model embodiment is clearly and completely described, it is clear that described
Embodiment is only a part of the embodiment of the utility model, instead of all the embodiments.Based on the implementation in the utility model
Example, all other embodiment obtained by those of ordinary skill in the art without making creative efforts belong to
The range of the utility model protection.
Referring to Fig. 1, the utility model embodiment includes:
A kind of guided missile Zhen Ci housing into rotation mechanism, comprising: body 1, taper die 2, plug 4, plug pedestal 5, cone rotation
Rotating motor 6 and cone oscillating motor 7 are provided with plug pedestal 5 on the body 1, and described 4 one end of plug is arranged with taper die
2,4 other end of plug is connect with plug pedestal 5, is provided with cone rotating electric machine 6 and cone oscillating motor on the body 1
7, the cone rotating electric machine 6 is sequentially connected with plug pedestal 5, and 4 bottom end of plug is arranged with plug set, and the cone is swung
Motor 7 and plug set are sequentially connected, and are provided with missile case 3 on the taper die 2.
1 side of body is provided with cone support base 8, and the cone support base 8 includes support screw 81 and support plate
82, the top of the support plate 82 and support screw 81 is connected by shaft 83.
The cone rotating electric machine 6 and cone oscillating motor 7 are connect with step-by-step control system.
When it is implemented, cone rotating electric machine 6 and plug pedestal 5 are sequentially connected, to drive the rotation of plug 4, in turn
Realize the 360 degree rotation of taper die 2, the bottom end of the plug 4 is also cased with plug set, and cone oscillating motor 7 and plug set pass
Dynamic connection to drive the swing of plug 4, and then realizes that the 180 degree of taper die 2 is swung, and 1 side of body is provided with cone
Body support base 8, the support plate 82 on cone support base 8 are used to support the missile case 3 on setting taper die 2.
In conclusion a kind of guided missile Zhen Ci housing into rotation mechanism that the utility model is pointed out, substitution is artificial, pierces and processes in needle
When carbon fiber, straight forming guided missile body, fiber fleece uniformity is good, can satisfy the production requirement of guided missile quality.
The above description is only the embodiments of the present invention, and therefore it does not limit the scope of the patent of the utility model, all
Using equivalent structure or equivalent flow shift made by the utility model description, it is applied directly or indirectly in other phases
The technical field of pass, is also included in the patent protection scope of the utility model.
Claims (5)
1. a kind of guided missile Zhen Ci housing into rotation mechanism characterized by comprising body, taper die, plug, plug pedestal, cone
Body rotating electric machine and cone oscillating motor are provided with plug pedestal on the body, and described plug one end is arranged with taper die,
The plug other end is connect with plug pedestal, and cone rotating electric machine and cone oscillating motor are provided on the body, described
Cone rotating electric machine is connect with plug base drive, and the plug bottom end is arranged with plug set, the cone oscillating motor and core
Stick set is sequentially connected, and is provided with missile case on the taper die.
2. guided missile Zhen Ci housing into rotation mechanism according to claim 1, which is characterized in that the taper die can carry out
360 degree rotation.
3. guided missile Zhen Ci housing into rotation mechanism according to claim 1, which is characterized in that the taper die can carry out
180 swing.
4. guided missile Zhen Ci housing into rotation mechanism according to claim 1, which is characterized in that the cone rotating electric machine and cone
Body oscillating motor is connect with step-by-step control system.
5. guided missile Zhen Ci housing into rotation mechanism according to claim 1, which is characterized in that the body side is provided with cone
Body support base, the cone support base include support screw and support plate, and the top of the support plate and support screw is by turning
Axis connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821810989.2U CN209246818U (en) | 2018-11-05 | 2018-11-05 | A kind of guided missile Zhen Ci housing into rotation mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821810989.2U CN209246818U (en) | 2018-11-05 | 2018-11-05 | A kind of guided missile Zhen Ci housing into rotation mechanism |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209246818U true CN209246818U (en) | 2019-08-13 |
Family
ID=67527169
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821810989.2U Active CN209246818U (en) | 2018-11-05 | 2018-11-05 | A kind of guided missile Zhen Ci housing into rotation mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209246818U (en) |
-
2018
- 2018-11-05 CN CN201821810989.2U patent/CN209246818U/en active Active
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