CN204221369U - The two main shaft turning-milling complex processing lathe of aeroplane engine casing processing - Google Patents
The two main shaft turning-milling complex processing lathe of aeroplane engine casing processing Download PDFInfo
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- CN204221369U CN204221369U CN201420713615.4U CN201420713615U CN204221369U CN 204221369 U CN204221369 U CN 204221369U CN 201420713615 U CN201420713615 U CN 201420713615U CN 204221369 U CN204221369 U CN 204221369U
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- lathe
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- milling complex
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Abstract
The utility model provides a kind of aeroplane engine casing to process with two main shaft turning-milling complex processing lathe, and the horizontal axis ram for laterally processing casing is equipped with by cross slid platform in the external side of bed, is provided with main slide unit below bed body.The utility model, by above-mentioned setting like this, can carry out turning-milling complex processing that is vertical and laterally two directions to profile inside and outside aeroplane engine casing, favourable raising machining accuracy and work efficiency simultaneously.
Description
Technical field
The utility model relates to the lathe that the processing of a kind of aeroplane engine casing uses, specifically the two main shaft turning-milling complex processing lathe of a kind of aeroplane engine casing processing.
Background technology
The required precision of each component processing of aero-engine is very high, and starts casing to be the pedestal of whole engine, and its inside is main shaft and blade, outsidely connects each component, comprises oil pipe, cooling tube and control system, have complex-shaped and material is special, and overall thin-walled, its car, the operation of Milling Machining is very complicated, particularly single operation car, it is long that the cycle is cut in milling, general first with the surfaces externally and internally of vertical lathe to casing and the mounting edge of front and back at present, the positions such as cannelure are sequentially carried out rough turn, half finish turning, finish turning is processed, then to rough mill casing with three axis machining center and the brill of installing hole limit and radial hole, expand, fraising, finally again with Five-axis NC Machining Center to mount pad, boss, laces etc. carry out finish-milling processing, and this traditional technique needs three class distinct devices altogether, and front and back mount and dismount for 12 times totally on different devices, cause that to relate to equipment many thus, flow process is complicated, being dismounted for multiple times causes position error large, and precision is difficult to ensure, directly affects crudy, simultaneously more than 360 hours consuming time of whole set process flow process, and efficiency is extremely low.
Summary of the invention
The purpose of this utility model is to solve above-mentioned complex procedures, relate to equipment many, affect machining accuracy and the problems such as work efficiency is low, a kind of aeroplane engine casing is provided to process with two main shaft turning-milling complex processing lathe, can once machine each operation, precision is high, work efficiency is fast simultaneously.
The utility model comprises the bed body of lathe, slide unit body crossbeam above bed body is equipped with, this slide unit body is configured with the vertical shaft ram for vertically processing casing, the technical scheme adopted is: by cross slid platform, the horizontal axis ram for laterally processing casing is housed in the external side of bed, bed body bottom is provided with main slide unit.
In technique scheme: described cross slid platform is arranged on the guide rail of the external side of bed.
Be equipped with above the main slide unit of bed body bottom for clamping and the cradle-type panoramic table regulating casing spatial attitude, move Milling Process to realize two main shaft seven coordinate 5-linked.And when cradle-type panoramic table be in horizontal attitude and locked do not swing time, rotated by panoramic table and can realize two main shaft turnery processing simultaneously.
Described bed body is a portal frame type structure.
The utility model compared with prior art has following good effect: by above-mentioned so a kind of technical scheme, owing to have employed the structure of installed vertical and horizontal ram simultaneously on the lathe body of a gantry frame structure, arrange below bed body simultaneously coordinate with it processing for clamping and the cradle-type panoramic table regulating casing, the disposable car simultaneously completing each operation at a machine tool can be realized, Milling Machining, owing to decreasing the processes such as repeated disassembled and assembled moves, the cooperatively interacting of machining tool makes it machining accuracy and working (machining) efficiency improves greatly, solve current manufacturing procedure thus complicated, relate to equipment and repeated disassembled and assembled workpiece and affect machining accuracy and the low problems of work efficiency, the total quality of favourable raising workpiece.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the utility model is described in further detail.
Fig. 1 is structural representation of the present utility model.
In figure: 1, bed body, 2, crossbeam, 3, slide unit body, 4, vertical shaft ram, 5, horizontal axis ram, 6, cross slid platform, 7, guide rail, 8, cradle-type panoramic table, 9, main slide unit.
Detailed description of the invention
Shown in Fig. 1: by cross slid platform 6, the horizontal axis ram 5 for laterally processing casing being housed outside bed body 1, being provided with main slide unit 9 below bed body 1.Cross slid platform 6 is arranged on the guide rail 7 outside a body 1.Be equipped with for clamping and the cradle-type panoramic table 8 regulating casing spatial attitude above main slide unit 9 below bed body 1.Bed body 1 is a portal frame type structure.
Claims (4)
1. the two main shaft turning-milling complex processing lathe of aeroplane engine casing processing, comprise the bed body (1) of lathe, the crossbeam (2) of bed body (1) top is equipped with slide unit body (3), this slide unit body (3) is configured with the vertical shaft ram (4) for vertically processing casing, it is characterized in that: the horizontal axis ram (5) for laterally processing casing is equipped with by cross slid platform (6) in bed body (1) outside, and bed body (1) below is provided with main slide unit (9).
2. the two main shaft turning-milling complex processing lathe of aeroplane engine casing processing according to claim 1, is characterized in that: described cross slid platform (6) is arranged on the guide rail (7) in a body (1) outside.
3. the two main shaft turning-milling complex processing lathe of aeroplane engine casing processing according to claim 1, it is characterized in that: main slide unit (9) top of bed body (1) below is equipped with for clamping and the cradle-type panoramic table (8) regulating casing spatial attitude, the topology requirement that two main shaft seven coordinate 5-linked moves turning-milling complex processing can be met.
4. the two main shaft turning-milling complex processing lathe of aeroplane engine casing processing according to claim 1, is characterized in that: described bed body (1) is a portal frame type structure.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420713615.4U CN204221369U (en) | 2014-11-18 | 2014-11-18 | The two main shaft turning-milling complex processing lathe of aeroplane engine casing processing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420713615.4U CN204221369U (en) | 2014-11-18 | 2014-11-18 | The two main shaft turning-milling complex processing lathe of aeroplane engine casing processing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204221369U true CN204221369U (en) | 2015-03-25 |
Family
ID=52919511
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420713615.4U Expired - Fee Related CN204221369U (en) | 2014-11-18 | 2014-11-18 | The two main shaft turning-milling complex processing lathe of aeroplane engine casing processing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204221369U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104802039A (en) * | 2015-04-28 | 2015-07-29 | 佛山市普拉迪数控科技有限公司 | Novel numerical control machine tool for multi-axial polyhedral machining function |
| CN104802013A (en) * | 2015-04-28 | 2015-07-29 | 佛山市普拉迪数控科技有限公司 | Multi-surface processing numerical control processing center |
| CN104827353A (en) * | 2015-04-28 | 2015-08-12 | 佛山市普拉迪数控科技有限公司 | Numerical control machining center with multi-axis and multi-surface machining function |
| WO2024060103A1 (en) * | 2022-09-21 | 2024-03-28 | 中国科学院深圳先进技术研究院 | Numerical control machine tool |
-
2014
- 2014-11-18 CN CN201420713615.4U patent/CN204221369U/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104802039A (en) * | 2015-04-28 | 2015-07-29 | 佛山市普拉迪数控科技有限公司 | Novel numerical control machine tool for multi-axial polyhedral machining function |
| CN104802013A (en) * | 2015-04-28 | 2015-07-29 | 佛山市普拉迪数控科技有限公司 | Multi-surface processing numerical control processing center |
| CN104827353A (en) * | 2015-04-28 | 2015-08-12 | 佛山市普拉迪数控科技有限公司 | Numerical control machining center with multi-axis and multi-surface machining function |
| CN104827353B (en) * | 2015-04-28 | 2018-08-10 | 佛山市普拉迪数控科技有限公司 | A kind of numerical control machining center of multiaxis multi-panel processing |
| WO2024060103A1 (en) * | 2022-09-21 | 2024-03-28 | 中国科学院深圳先进技术研究院 | Numerical control machine tool |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150325 Termination date: 20151118 |