CN203210187U - Deburring device for aeronautical parts - Google Patents
Deburring device for aeronautical parts Download PDFInfo
- Publication number
- CN203210187U CN203210187U CN 201320250756 CN201320250756U CN203210187U CN 203210187 U CN203210187 U CN 203210187U CN 201320250756 CN201320250756 CN 201320250756 CN 201320250756 U CN201320250756 U CN 201320250756U CN 203210187 U CN203210187 U CN 203210187U
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- CN
- China
- Prior art keywords
- deburring device
- crossbeam
- cantilever beam
- jet
- water
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- Expired - Fee Related
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Abstract
The utility model provides a deburring device for aeronautical parts. The deburring device is capable of removing burrs on machined parts and applicable to the technical field of aeronautical machining. The deburring device comprises a workbench, columns are arranged on the workbench, a crossbeam capable of moving longitudinally along the columns is supported on the columns, a cantilever beam capable of moving transversely along the crossbeam is supported on the crossbeam, and a group of water-sediment jet nozzles capable of moving transversely along the cantilever beam are mounted below the cantilever beam, and inflow ends of the nozzles are connected with a water-sediment jet source externally. A high-pressure water jet cutter cutting technology is used for reference, and water-sediment jet is adopted for removing the burrs of the aeronautical parts accurately; the deburring device is good in removing effect, high in working efficiency, capable of saving energy and environmentally friendly; compared with an abrasive polishing method, the deburring device has the advantages that abrasive is saved, and economic benefit is improved; meanwhile, dust and noise can be eliminated, working environment is improved, good health of workers is benefitted, and the deburring device conforms to current green and environment-friendly trends.
Description
Technical field
The utility model proposes a kind of aviation part burr remover, can remove the burr on the part after the machining, be applicable to the aviation machine processing technique field.
Background technology
Usually, the machinability of aeronautical material is all poor, such as the titanium alloy of aerospace field extensive use, and nickel base superalloy etc., its intensity, toughness, hardness are stayed the extremely difficult removal of burr on the part all than higher after the processing.In actual production process, need the professional to remove with sand paper, abrasive band, file etc. are manual at the deburring station, it is low to remove efficient, and poor quality.
Occurred some high-pressure spray flash trimmers in the market, but because the restriction of its pressure and working media generally can only be used for the burr that removal intensity, toughness are hanged down material, to the deburring effect after the aviation part processing and bad.
Need the burr remover of developing at the aviation part badly.
The utility model content
The utility model will be realized following purpose: for solving the problem that prior art exists, propose a kind of aviation part burr remover, can effectively remove the burr on the aviation part.
For realizing above purpose, the technical solution of the utility model is as follows:
A kind of aviation part burr remover, comprise workbench, it is characterized in that, described workbench is provided with column, described column upper support has the crossbeam that can vertically move along column, described crossbeam upper support has can be along the horizontal mobile cantilever beam of crossbeam, and being equipped with one group under the described cantilever beam can be along the husky fluid jet nozzle of the water that cantilever beam laterally moves; The husky jet source of the outer water receiving of the influent stream end of described shower nozzle.
Preferably, also be provided with protective baffle plate on the described workbench.More preferably, described protective baffle plate is for splitting movable structure.
Preferably, described workbench is the hollow header tank that the top has leaking hole.
Preferably, the husky jet source of described water is for mixing current and producing the high-pressure spray pump that pressure is at least the jet of 30Mpa with fine sand.
The utility model is used for reference the high-pressure water knife cutting technique, adopt the husky jet of water that the aviation part is accurately removed burr, removal effect is good, high efficiency, energy-conserving and environment-protective, compared to the way that adopts the abrasive material polishing, not only save abrasive material but also improved economic benefit, can eliminate the dust noise simultaneously, improved operating environment, be conducive to the healthy of operating worker, meet the trend of current environmental protection.
Description of drawings
Fig. 1 is the structural representation of the utility model embodiment.
The specific embodiment
Embodiment
The aviation part burr remover basic structure of present embodiment as shown in Figure 1, comprise workbench 1, workbench 1 is provided with column 2, column 2 upper supports have the crossbeam 3 that can vertically move along column 2, crossbeam 3 upper supports have can be along crossbeam 3 horizontal mobile cantilever beams 4, and cantilever beam is equipped with one group for 4 times can be along the husky fluid jet nozzles 5 of the water that cantilever beam 4 laterally moves; The husky jet source (not shown) of the outer water receiving of the influent stream end of shower nozzle.
In addition, also be provided with protective baffle plate 6 on the workbench 1.Workbench 1 has the hollow header tank of leaking hole (not shown) for the top.The husky jet source of water is for mixing current and producing the high-pressure spray pump (not shown) that pressure is at least the jet of 30Mpa with fine sand.
Specific implementation process is as follows:
To those skilled in the art, under the prerequisite that does not break away from the utility model technical conceive, any equivalent transformation scheme of making and be equal to replacement scheme all belongs to the scope of the utility model claim protection.
Claims (5)
1. aviation part burr remover, comprise workbench, it is characterized in that, described workbench is provided with column, described column upper support has the crossbeam that can vertically move along column, described crossbeam upper support has can be along the horizontal mobile cantilever beam of crossbeam, and being equipped with one group under the described cantilever beam can be along the husky fluid jet nozzle of the water that cantilever beam laterally moves; The husky jet source of the outer water receiving of the influent stream end of described shower nozzle.
2. aviation part burr remover according to claim 1 is characterized in that, also is provided with protective baffle plate on the described workbench.
3. aviation part burr remover according to claim 2 is characterized in that described protective baffle plate is for splitting movable structure.
4. aviation part burr remover according to claim 3 is characterized in that, described workbench is the hollow header tank that the top has leaking hole.
5. aviation part burr remover according to claim 4 is characterized in that, the husky jet source of described water is for mixing current and producing the high-pressure spray pump that pressure is at least the jet of 30Mpa with fine sand.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320250756 CN203210187U (en) | 2013-05-09 | 2013-05-09 | Deburring device for aeronautical parts |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201320250756 CN203210187U (en) | 2013-05-09 | 2013-05-09 | Deburring device for aeronautical parts |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203210187U true CN203210187U (en) | 2013-09-25 |
Family
ID=49199757
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201320250756 Expired - Fee Related CN203210187U (en) | 2013-05-09 | 2013-05-09 | Deburring device for aeronautical parts |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203210187U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108081156A (en) * | 2017-12-26 | 2018-05-29 | 安徽开诚电器有限公司 | A kind of mold polish device |
| CN112951747A (en) * | 2021-03-21 | 2021-06-11 | 新恒通(江苏)科技有限公司 | Combined appliance of chip burr etching machine |
| CN112951747B (en) * | 2021-03-21 | 2024-05-14 | 新恒通(江苏)科技有限公司 | Combined device of chip burr etching machine |
-
2013
- 2013-05-09 CN CN 201320250756 patent/CN203210187U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108081156A (en) * | 2017-12-26 | 2018-05-29 | 安徽开诚电器有限公司 | A kind of mold polish device |
| CN112951747A (en) * | 2021-03-21 | 2021-06-11 | 新恒通(江苏)科技有限公司 | Combined appliance of chip burr etching machine |
| CN112951747B (en) * | 2021-03-21 | 2024-05-14 | 新恒通(江苏)科技有限公司 | Combined device of chip burr etching machine |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130925 Termination date: 20140509 |