CN219805589U - Welding positioning die for aviation components - Google Patents
Welding positioning die for aviation components Download PDFInfo
- Publication number
- CN219805589U CN219805589U CN202320027315.XU CN202320027315U CN219805589U CN 219805589 U CN219805589 U CN 219805589U CN 202320027315 U CN202320027315 U CN 202320027315U CN 219805589 U CN219805589 U CN 219805589U
- Authority
- CN
- China
- Prior art keywords
- spring
- fixedly connected
- aviation
- bottom plate
- positioning die
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Links
- 238000003466 welding Methods 0.000 title claims abstract description 20
- 238000004519 manufacturing process Methods 0.000 abstract description 7
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000012994 industrial processing Methods 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
Landscapes
- Moulds For Moulding Plastics Or The Like (AREA)
Abstract
The utility model provides a welding positioning die for an aviation component, and relates to the field of aviation component production. The welding positioning die for the aviation component comprises a bottom plate, wherein a first spring is fixedly connected to the upper surface of the bottom plate, a fixed block is fixedly connected to the top end of the first spring, a positioning frame is fixedly connected to the right side of the fixed block, a pressing plate is fixedly connected to the inner wall of the positioning frame, a movable hole communicated with the inside of the positioning frame is formed in the left side of the positioning frame, and a movable rod is movably connected to the inside of the movable hole. This aviation part's welding position mould, through bottom plate, lifting hole, gag lever post, first spring, fixed block, movable rod, movable hole, second spring, clamp plate, mutually supporting between limiting plate and the locating frame, reach and be convenient for extrude fixedly each other with two parts for the welded part is inseparabler, has solved current aviation part welding position mould and is difficult for carrying out two parts mutually fixed, thereby influences the problem of welded part compactness.
Description
Technical Field
The utility model relates to the technical field of aviation component production, in particular to a welding positioning die for aviation components.
Background
The aviation parts manufacturing industry mainly refers to the manufacture of various parts of aviation aircrafts. Including aircraft organism spare part manufacturing, aeroengine spare part manufacturing, instrument, airborne equipment, hydraulic system and manufacturing such as annex, do not include spare part assembly, aeroengine assembly and complete machine assembly etc. the aeronautical parts is the same with other industrial processing, all need utilize positioning die to carry out the part location, avoid influencing the processing effect, current aeronautical parts welding positioning die is difficult to carry out two parts and fix each other to influence weld compactness.
Disclosure of Invention
The utility model aims to provide a welding positioning die for an aviation component, which solves the problem that the existing welding positioning die for the aviation component is difficult to fix two parts to each other, so that the compactness of a welding position is affected.
Technical proposal
In order to achieve the above purpose, the utility model is realized by the following technical scheme: the utility model provides a welding positioning die of aviation part, includes the bottom plate, the upper surface fixedly connected with first spring of bottom plate, the top fixedly connected with fixed block of first spring, the right side fixedly connected with locating frame of fixed block, the inner wall fixedly connected with clamp plate of locating frame, the movable hole that is linked together with locating frame inside has been seted up in the left side of locating frame, the inside swing joint in movable hole has the movable rod, the right-hand member fixedly connected with limiting plate of movable rod, the second spring has been cup jointed on the surface of movable rod, the left end and the inner wall fixedly connected with of locating frame of second spring, the right-hand member and the left side fixedly connected of limiting plate of second spring.
Further, the lifting hole communicated with the lower surface is formed in the upper surface of the bottom plate, a limiting rod is movably connected in the lifting hole, and the top end of the limiting rod is fixedly connected with the lower surface of the fixed block.
Further, the first spring is sleeved on the outer surface of the limiting rod.
Further, the number of the pressing plates is two, and the two pressing plates are symmetrically arranged on the central axis of the positioning frame.
The utility model provides a welding positioning die for an aviation component. The beneficial effects are as follows:
this aviation part's welding position mould, through bottom plate, lifting hole, gag lever post, first spring, fixed block, movable rod, movable hole, second spring, clamp plate, mutually supporting between limiting plate and the locating frame, reach and be convenient for extrude fixedly each other with two parts for the welded part is inseparabler, has solved current aviation part welding position mould and is difficult for carrying out two parts mutually fixed, thereby influences the problem of welded part compactness.
Drawings
FIG. 1 is a schematic diagram of the structure of the present utility model;
fig. 2 is a front view of the structure of the present utility model.
Wherein, 1 bottom plate, 2 lifting hole, 3 gag lever post, 4 first springs, 5 fixed blocks, 6 movable rod, 7 movable hole, 8 second springs, 9 clamp plates, 10 limiting plates, 11 locating frame.
Detailed Description
As shown in fig. 1-2, the embodiment of the utility model provides a welding positioning die for aviation components, which comprises a bottom plate 1, wherein the upper surface of the bottom plate 1 is fixedly connected with a first spring 4, the top end of the first spring 4 is fixedly connected with a fixed block 5, the upper surface of the bottom plate 1 is provided with a lifting hole 2 communicated with the lower surface, the inside of the lifting hole 2 is movably connected with a limiting rod 3, the top end of the limiting rod 3 is fixedly connected with the lower surface of the fixed block 5, the first spring 4 is positioned on the outer surface of the limiting rod 3 in a sleeving manner, the right side of the fixed block 5 is fixedly connected with a positioning frame 11, the inner wall of the positioning frame 11 is fixedly connected with two pressing plates 9, the two pressing plates 9 are symmetrically arranged with the central axis of the positioning frame 11, the left side of the positioning frame 11 is provided with a movable hole 7 communicated with the inside of the positioning frame 11, the inside of the movable hole 7 is movably connected with a movable rod 6, the right end of the movable rod 6 is fixedly connected with a limiting plate 10, the surface of the movable rod 6 is sleeved with a second spring 8, the left end of the second spring 8 is fixedly connected with the inner wall of the positioning frame 11 in a sleeving manner, and the right end of the second spring 8 is fixedly connected with the left side of the limiting plate 10.
Working principle: the two moving rods 6 are oppositely pulled, the positioning frame 11 is pulled upwards, then the two parts are butted and placed on the surface of the bottom plate 1, then the positioning frame 11 is released, the first spring 4 is contracted to drive the fixed block 5 to move downwards, the fixed block 5 drives the positioning frame 11 to move downwards, the two pressing plates 9 press the two parts downwards, then the two moving rods 6 are released, and at the moment, the two second springs 8 relatively push the limiting plate 10 to press the two parts to each other, so that the joint of the two parts is tighter.
Claims (4)
1. Welding positioning die for aviation components, comprising a bottom plate (1), and being characterized in that: the utility model discloses a movable structure of a floor, including bottom plate (1), fixed block (5), locating frame (11), movable hole (7) and locating frame (11) inside be linked together are offered in the left side of locating frame (11), movable hole (7)'s inside swing joint has movable rod (6), movable rod (6)'s right-hand member fixedly connected with limiting plate (10), second spring (8) have been cup jointed on the surface of movable rod (6), the left end of second spring (8) and locating frame (11)'s inner wall fixed connection, the right-hand member and the left side fixed connection of limiting plate (10) of second spring (8).
2. The welding positioning die for aviation components of claim 1, wherein: lifting holes (2) communicated with the lower surface are formed in the upper surface of the bottom plate (1), limiting rods (3) are movably connected in the lifting holes (2), and the top ends of the limiting rods (3) are fixedly connected with the lower surface of the fixed block (5).
3. The welding positioning die for aviation components of claim 2, wherein: the first spring (4) is positioned on the outer surface of the limiting rod (3) in a sleeved mode.
4. The welding positioning die for aviation components of claim 1, wherein: the number of the pressing plates (9) is two, and the two pressing plates (9) are symmetrically arranged on the central axis of the positioning frame (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320027315.XU CN219805589U (en) | 2023-01-06 | 2023-01-06 | Welding positioning die for aviation components |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202320027315.XU CN219805589U (en) | 2023-01-06 | 2023-01-06 | Welding positioning die for aviation components |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN219805589U true CN219805589U (en) | 2023-10-10 |
Family
ID=88214628
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202320027315.XU Active CN219805589U (en) | 2023-01-06 | 2023-01-06 | Welding positioning die for aviation components |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN219805589U (en) |
-
2023
- 2023-01-06 CN CN202320027315.XU patent/CN219805589U/en active Active
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Legal Events
| Date | Code | Title | Description |
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| GR01 | Patent grant | ||
| GR01 | Patent grant |