CN204449748U - A kind of Flight Vehicle Structure part welding positioning clamp - Google Patents
A kind of Flight Vehicle Structure part welding positioning clamp Download PDFInfo
- Publication number
- CN204449748U CN204449748U CN201520024187.9U CN201520024187U CN204449748U CN 204449748 U CN204449748 U CN 204449748U CN 201520024187 U CN201520024187 U CN 201520024187U CN 204449748 U CN204449748 U CN 204449748U
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- China
- Prior art keywords
- locating surface
- clamping area
- vehicle structure
- flight vehicle
- structure part
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Abstract
The utility model discloses a kind of Flight Vehicle Structure part welding positioning clamp, comprise positioning support, slide block and screw rod, positioning support is provided with the first locating surface, second locating surface and screw rod erecting bed, first locating surface and the second locating surface are arranged in setting angle, screw rod erecting bed is provided with the screwed hole worn for screw rod, the lower end of screw rod is fixedly installed slide block, slide block is provided with the first clamping area and the second clamping area, first locating surface and the first clamping area are parallel to each other, second locating surface and the second clamping area are parallel to each other, Flight Vehicle Structure part to be welded is placed on the first locating surface and the first clamping area respectively, between second locating surface and the second clamping area, locating surface is made by moving down slide block, clamping area mutually clamps and fixes Flight Vehicle Structure part, it is made to be the welding of setting angle.The square steel that the utility model is applicable to the medium-sized frame-saw frame of Flight Vehicle Structure is located, steps up, is ensured that angle is welded, and improves location and the clamping of square steel, improves welding efficiency.
Description
Technical field
The utility model belongs to frock assisted class frock, is specifically related to a kind of Flight Vehicle Structure part welding positioning clamp.
Background technology
Relate to the welding of various structures form, multiple angles in Flight Vehicle Structure part, these welding all need to reach certain precision.But in practical operation, angle welding operation difficulty, welding efficiency are very low, are difficult to the precision ensureing angle welding.
Utility model content
For prior art Problems existing, the purpose of this utility model is to provide a kind of and improves welding efficiency, meet the Flight Vehicle Structure part welding positioning clamp of multi-angle welding.
For achieving the above object, a kind of Flight Vehicle Structure part of the utility model welding positioning clamp, comprise positioning support, slide block and screw rod, positioning support is provided with the first locating surface, second locating surface and screw rod erecting bed, first locating surface and the second locating surface are arranged in setting angle according to user demand, screw rod erecting bed is provided with the screwed hole worn for screw rod, the lower end of screw rod is fixedly installed slide block, this slide block is provided with the first clamping area and the second clamping area, wherein, first locating surface and the first clamping area are parallel to each other, second locating surface and the second clamping area are parallel to each other, Flight Vehicle Structure part to be welded is placed on the first locating surface and the first clamping area respectively, between second locating surface and the second clamping area, locating surface is made by moving down slide block, clamping area mutually clamps and fixes Flight Vehicle Structure part, it is made to be the welding of setting angle.
Further, described setting angle is 0-180 degree.
Further, described setting angle is 90 degree.
Further, described Flight Vehicle Structure part is square steel material.
The utility model welding positioning clamp, the square steel being highly suitable for the medium-sized frame-saw frame of Flight Vehicle Structure is located, steps up, is ensured that angle is welded, greatly improve location and the clamping of square steel, improve welding efficiency greatly simultaneously, there is larger actual application value.
Accompanying drawing explanation
Fig. 1 is the utility model structural representation;
Wherein Reference numeral is: 1-positioning support, 2-slide block, 3-screw rod, 4-first locating surface, 5-second locating surface, 6-screw rod erecting bed, 7-first clamping area, 8-second clamping area.
Detailed description of the invention
Below, with reference to accompanying drawing, the utility model is more fully illustrated, shown in the drawings of exemplary embodiment of the present utility model.But the utility model can be presented as multiple multi-form, and should not be construed as the exemplary embodiment being confined to describe here.But, these embodiments are provided, thus make the utility model comprehensively with complete, and scope of the present utility model is fully conveyed to those of ordinary skill in the art.
For ease of illustrating, here can use such as " on ", the space relative terms such as D score " left side " " right side ", for illustration of the element of shown in figure or the feature relation relative to another element or feature.It should be understood that except the orientation shown in figure, spatial terminology is intended to comprise device different azimuth in use or operation.Such as, if the device in figure is squeezed, be stated as the element being positioned at other elements or feature D score will be positioned at other elements or feature " on ".Therefore, exemplary term D score can comprise upper and lower both orientation.Device can otherwise be located (90-degree rotation or be positioned at other orientation), and space used here illustrates relatively can correspondingly explain.
As shown in Figure 1, a kind of Flight Vehicle Structure part of the utility model welding positioning clamp, comprise positioning support 1, slide block 2 and screw rod 3, positioning support 1 is provided with the first locating surface 4, second locating surface 5 and screw rod erecting bed 6, first locating surface 4 and the second locating surface 5 are arranged in setting angle according to user demand, screw rod erecting bed 6 is provided with the screwed hole worn for screw rod 3, the lower end of screw rod 3 is fixedly installed slide block 2, this slide block 2 is provided with the first clamping area 7 and the second clamping area 8, wherein, first locating surface 4 and the first clamping area 7 are parallel to each other, second locating surface 5 and the second clamping area 8 are parallel to each other, Flight Vehicle Structure part to be welded is placed on the first locating surface 4 and the first clamping area 7 respectively, between second locating surface 5 and the second clamping area 8, locating surface is made by moving down slide block 2, clamping area mutually clamps and fixes Flight Vehicle Structure part, it is made to be the welding of setting angle.
Setting angle between first locating surface 4 and the second locating surface 5 can be set to 0-180 degree according to user demand.Flight Vehicle Structure part is generally square steel material.
The first locating surface 4 shown in Fig. 1 and the setting angle between the second locating surface 5 are 90 degree, and it forms two fixing right angle locating surfaces.Setting angle between first clamping area 7 and the second clamping area 8 is also 90 degree, and it forms two fixing right angle clamping areas.During work, by the rotation forces movable sliding block 2 of screw rod 3, thus realize stepping up and locating and ensure vertical process of two square steel, ensure the reliability that two square steel are vertical.The structure of this welding positioning clamp makes square steel be easy to be located and clamp on frock framework and ensures the process of vertical welding.Utilize this welding positioning clamp greatly can improve the welding quality of frock framework, also effectively can ensure perpendicularity between each square steel simultaneously and be applicable to the square steel of all size.
For the described setting angle of other angles, its basic structure form is identical with structure shown in Fig. 1, the setting angle of 0-180 degree is arranged, multiple welding demand can be met, greatly improve convenience, the high efficiency of Flight Vehicle Structure part welding, ensure that high welding quality, there is larger actual application value.
Claims (4)
1. a Flight Vehicle Structure part welding positioning clamp, it is characterized in that, comprise positioning support, slide block and screw rod, positioning support is provided with the first locating surface, second locating surface and screw rod erecting bed, first locating surface and the second locating surface are arranged in setting angle according to user demand, screw rod erecting bed is provided with the screwed hole worn for screw rod, the lower end of screw rod is fixedly installed slide block, this slide block is provided with the first clamping area and the second clamping area, wherein, first locating surface and the first clamping area are parallel to each other, second locating surface and the second clamping area are parallel to each other, Flight Vehicle Structure part to be welded is placed on the first locating surface and the first clamping area respectively, between second locating surface and the second clamping area, locating surface is made by moving down slide block, clamping area mutually clamps and fixes Flight Vehicle Structure part, it is made to be the welding of setting angle.
2. Flight Vehicle Structure part welding positioning clamp as claimed in claim 1, it is characterized in that, described setting angle is 0-180 degree.
3. Flight Vehicle Structure part welding positioning clamp as claimed in claim 2, it is characterized in that, described setting angle is 90 degree.
4. Flight Vehicle Structure part welding positioning clamp as claimed in claim 1, it is characterized in that, described Flight Vehicle Structure part is square steel material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520024187.9U CN204449748U (en) | 2015-01-14 | 2015-01-14 | A kind of Flight Vehicle Structure part welding positioning clamp |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520024187.9U CN204449748U (en) | 2015-01-14 | 2015-01-14 | A kind of Flight Vehicle Structure part welding positioning clamp |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204449748U true CN204449748U (en) | 2015-07-08 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520024187.9U Active CN204449748U (en) | 2015-01-14 | 2015-01-14 | A kind of Flight Vehicle Structure part welding positioning clamp |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204449748U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107127507A (en) * | 2017-06-19 | 2017-09-05 | 绵竹市加林动力备件厂（普通合伙） | It is conveniently adjusted the weld clamp method of weldment angle |
| CN107160078A (en) * | 2017-06-19 | 2017-09-15 | 绵竹市加林动力备件厂（普通合伙） | A kind of fixing device for improving steam turbine pipeline welding quality |
-
2015
- 2015-01-14 CN CN201520024187.9U patent/CN204449748U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107127507A (en) * | 2017-06-19 | 2017-09-05 | 绵竹市加林动力备件厂（普通合伙） | It is conveniently adjusted the weld clamp method of weldment angle |
| CN107160078A (en) * | 2017-06-19 | 2017-09-15 | 绵竹市加林动力备件厂（普通合伙） | A kind of fixing device for improving steam turbine pipeline welding quality |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20160804 Address after: 109 box 49, box 333002 (Lv Meng factory area), Jingdezhen, Jiangxi Patentee after: Jingdezhen Changhang Aviation High-Tech Co., Ltd. Address before: 333002 No. 539 Chaoyang Road, Jiangxi, Jingdezhen Patentee before: Jiangxi Changhe Aviation Industries Co. Ltd |