CN103056615A - Processing process of array panel of array face frame parts - Google Patents
Processing process of array panel of array face frame parts Download PDFInfo
- Publication number
- CN103056615A CN103056615A CN 201210574441 CN201210574441A CN103056615A CN 103056615 A CN103056615 A CN 103056615A CN 201210574441 CN201210574441 CN 201210574441 CN 201210574441 A CN201210574441 A CN 201210574441A CN 103056615 A CN103056615 A CN 103056615A
- Authority
- CN
- China
- Prior art keywords
- front plate
- processing
- plate
- plane
- around
- 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.)
- Pending
Links
Images
Landscapes
- Heat Treatment Of Articles (AREA)
Abstract
The invention discloses a processing process of an array panel of array face frame parts. The process includes conducting coarse processing, vibration aging, semi-fine processing, manual aging, semi-fine processing, manual aging, fine processing and surface processing on the array panel of the array face frame parts to obtain an array panel of the finished array face frame parts. Due to the fact that the process adopts combination of vibration aging and hot processing manual aging and twice hot processing and manual aging, the process effectively resolves the problem of transformation in processing of large aluminum alloy panel pieces, overcomes the shortcoming of easiness in part abandonment in the traditional process scheme, improves part processing success rate and reduces cost.
Description
Technical field
The invention belongs to the machine components processing technique field, particularly relate to a kind of processing technology of front plate of front FRAME COMPONENTS.
Background technology
The forward and backward front plate of front FRAME COMPONENTS belongs to the large aluminum alloy flat part, and its appearance and size is large, thin thickness, middle drilling hole amount are extremely many, causes part very easily to deform in process, so that the higher dimensional requirement of part itself can't be guaranteed.
After existing processing technology adopts a roughing, carry out the heat treatment timeliness one time, then fine finishining moulding, this processing technology adopt less heat treatment number of times to guarantee the stable of part material, have avoided at high temperature separating out with destroyed of interior inner element of aluminum alloy materials.But, owing to only carried out Ageing Treatment one time, cause part internal stress and machining stress to discharge not exclusively, stress release after causing part owing to fine finishining produces distortion, yields is low, has caused like this premium of a large amount of parts, has improved greatly cost.
Summary of the invention
For the problems referred to above, the invention provides a kind of minimizing part deformation, improve the processing technology of front plate that part is processed into the front FRAME COMPONENTS of power.
For addressing the above problem, the technical scheme that the present invention takes is:
A kind of processing technology of front plate of front FRAME COMPONENTS, described this process may further comprise the steps:
1) uses planer-type milling machine hilted broadsword processing tool plate to see light to its plane, make its flatness be no more than 0.02mm;
2) after qualified the front plate is placed on the plane of the working plate after the processing and begins roughing, first around the processing, afterwards under nature, use hilted broadsword to mill after a plane sees light, upset front plate, mill another plane and see light, positive and negative respectively overturns and carries out milling twice, and (comprising chamfering) and two each faces of large plane stay 3mm allowance around the described front plate;
3) the front plate after the roughing is placed on the plane of the working plate after the processing, with gantry mill bore, bore hole, described bore hole by the center toward around, by three-back-shaped route bore, bore hole
4) the front plate behind the bore hole being carried out oscillating aging processes;
5) after oscillating aging was finished, panel poised for battle was smoothed, and guaranteed that flatness is less than 0.3mm;
6) get back to planer-type milling machine after the smoothing and carry out the semifinishing first time, first around the processing, afterwards the front plate is placed on the plane of the working plate after the processing, under nature, use hilted broadsword to be poised for battle the panel positive and negative and carry out milling, (comprising chamfering) and two large each face of face stay 2mm allowance around the described front plate;
7) the front plate reaming after for the first time semifinishing
8) the front plate compacting after the reaming is carried out heat treatment first time artificial aging at working plate, smoothing front plate after finishing guarantees that flatness is in 0.2mm;
9) get back to planer-type milling machine after the smoothing and carry out the secondary semifinishing, first around the processing, afterwards the front plate is placed on the plane of the working plate after the processing, under nature, use hilted broadsword to be poised for battle the panel positive and negative and carry out milling, (comprising chamfering) and two large each face of face stay 1mm allowance around the described front plate;
10) the front plate reaming after for the second time semifinishing
With in the middle of the front plate and periphery respectively organize aperture, counterbore and screwed hole bottom outlet and get out;
11) compacting of front plate is carried out heat treatment second time artificial aging at working plate, smoothing front plate after finishing guarantees flatness 0.15mm;
12) the front plate is carried out fine finishining, first around the processing, choose afterwards without the one side of counterbore and process under nature, then turn-over passes counterbore on the part with part compacting milling flat on working plate with screw, guarantees in size 12 ± 0.06 and the flatness 0.06mm;
13) the front plate after the fine finishining is carried out bore hole
Deburring after finishing, tapping.
14) get product after process on the surface of panel poised for battle.
As preferred version of the present invention, the working plate that described step 1) is used is cast iron plate.
As preferred version of the present invention, described each Kong Kongwei is by the final size tolerance, guarantees that tolerance is in ± 0.05mm.
As preferred version of the present invention, adopt the mode of Low Temperature Heat Treatment timeliness during described step 11) heat treatment timeliness, temperature is controlled at 180 ℃.
Because the present invention has adopted oscillating aging to be combined with the heat treatment artificial aging, twice heat treatment artificially aged processing technology, effectively solve the large aluminum alloy flat part and added the problem of being out of shape man-hour, solved the defective that past traditional handicraft scheme causes part to be scrapped easily, improve part and be processed into power, reduced cost.
Description of drawings
Fig. 1 is the front plate of processing technology processing of the present invention;
Route map when Fig. 2 is brill of the present invention, bore hole.
The specific embodiment
The invention will be further described below in conjunction with specific embodiment, is used for explaining the present invention in illustrative examples and the explanation of this invention, but not as a limitation of the invention.
The present invention includes following steps:
1) uses working plate to its plane of planer-type milling machine hilted broadsword processing cast iron plate to see light, make its flatness be no more than 0.02mm;
2) after qualified the front plate is placed on the plane of the working plate after the processing and begins roughing, first around the processing, afterwards under nature, use hilted broadsword to mill after a plane sees light, upset front plate, mill another plane and see light, positive and negative respectively overturns and carries out milling twice, and (comprising chamfering) and two each faces of large plane stay 3mm allowance around the described front plate;
3) the front plate after the roughing is placed on the plane of the working plate after the processing, carries out bore hole with Boring machine, described bore hole is by backward another direction straight line horizontal sliding of orientation determination benchmark, by the center toward around, by three-back-shaped route bore hole
This moment, each Kong Kongwei was by the final size tolerance, guaranteed that tolerance is in ± 0.05mm;
4) the front plate behind the bore hole being carried out oscillating aging processes;
5) after oscillating aging was finished, panel poised for battle was smoothed, and guaranteed that flatness is less than 0.3mm;
6) get back to planer-type milling machine after the smoothing and carry out the semifinishing first time, first around the processing, afterwards the front plate is placed on the plane of the working plate after the processing, under nature, use hilted broadsword panel positive and negative poised for battle respectively to overturn and carry out milling twice, (comprising chamfering) and two large each face of face stay 2mm allowance around the described front plate;
7) the front plate reaming after for the first time semifinishing
This moment, each Kong Kongwei was by the final size tolerance, guaranteed that tolerance is in ± 0.05mm;
8) the front plate compacting after the reaming is carried out heat treatment first time artificial aging at working plate, smoothing front plate after finishing guarantees that flatness is in 0.2mm;
9) get back to planer-type milling machine after the smoothing and carry out the secondary semifinishing, first around the processing, afterwards the front plate is placed on the plane of the working plate after the processing, under nature, use hilted broadsword panel positive and negative poised for battle respectively to overturn and carry out milling twice, (comprising chamfering) and two large each face of face stay 1mm allowance around the described front plate;
10) the front plate reaming after for the second time semifinishing
With in the middle of the front plate and periphery respectively organize aperture, counterbore and screwed hole bottom outlet and get out, this moment, each Kong Kongwei was by the final size tolerance, guaranteed that tolerance is in ± 0.05mm;
11) compacting of front plate is carried out heat treatment second time artificial aging at working plate, adopt the mode of Low Temperature Heat Treatment timeliness during the heat treatment timeliness, temperature is controlled at 180 ℃, and smoothing front plate after finishing guarantees flatness 0.15mm;
12) the front plate is carried out fine finishining, first around the processing, choose afterwards without the one side of counterbore and process under nature, then turn-over passes counterbore on the part with part compacting milling flat on working plate with screw, guarantees in size 12 ± 0.06 and the flatness 0.06mm;
13) the front plate after the fine finishining is carried out bore hole
Deburring after finishing, tapping.
14) get product after process on the surface of panel poised for battle.
As shown in Figure 1 and Figure 2, the front plate of processing technology processing of the present invention comprises front plate body 1, has on the front plate body 1
Bore hole 2, the direction of arrow that wherein indicates is the bore hole route, because front plate machining hole enormous amount for reducing to process the distortion of generation, is bored bore hole
Pre-hole
The time, for guaranteeing evenly to discharge stress, during bore hole by the center toward around, by three-back-shaped route.
The present invention has adopted the repeatedly mode of timeliness destressing, has effectively solved the large aluminum alloy flat part and has added the problem of being out of shape man-hour, has solved past traditional handicraft scheme and has caused easily the useless defective of front blackboard newspaper, has reduced cost.What shake simultaneously that timeliness and heat treatment artificially aged merge to use that for the second time heat treatment artificial aging adopts low temperature aging under little surplus has also effectively avoided the damage of material in heat treatment process; Oscillating aging is a kind of mode of eliminating the material internal stress, and it is fast to have speed, the characteristics that efficient is high, and the highest internal stress of removing part 80% in theory, and because oscillating aging need not heating, can avoid the problem that material element runs off in the heat treatment ag(e)ing process.
Technical scheme of the present invention is not limited to the restriction of above-mentioned specific embodiment, and the technology distortion that every technical scheme according to the present invention is made all falls within protection scope of the present invention.
Claims (4)
1. the processing technology of the front plate of a front FRAME COMPONENTS is characterized in that, described this process may further comprise the steps:
1) uses planer-type milling machine hilted broadsword processing tool plate to see light to its plane, make its flatness be no more than 0.02mm;
2) after qualified the front plate is placed on the plane of the working plate after the processing and begins roughing, first around the processing, afterwards under nature, use hilted broadsword to mill after a plane sees light, upset front plate, mill another plane and see light, positive and negative respectively overturns and carries out milling twice, and (comprising chamfering) and two each faces of large plane stay 3mm allowance around the described front plate;
3) the front plate after the roughing is placed on the plane of the working plate after the processing, with gantry mill bore, bore hole, described brill, bore hole by the center toward around, by three-back-shaped route bore, bore hole
4) the front plate behind the bore hole being carried out oscillating aging processes;
5) after oscillating aging was finished, panel poised for battle was smoothed, and guaranteed that flatness is less than 0.3mm;
6) get back to planer-type milling machine after the smoothing and carry out the semifinishing first time, first around the processing, afterwards the front plate is placed on the plane of the working plate after the processing, under nature, use hilted broadsword to be poised for battle the panel positive and negative and carry out milling, (comprising chamfering) and two large each face of face stay 2mm allowance around the described front plate;
7) the front plate reaming after for the first time semifinishing
8) the front plate compacting after the reaming is carried out heat treatment first time artificial aging at the special iron casting working plate, smoothing front plate after finishing guarantees that flatness is in 0.2mm;
9) get back to planer-type milling machine after the smoothing and carry out the secondary semifinishing, first around the processing, afterwards the front plate is placed on the plane of the working plate after the processing, under nature, use hilted broadsword to be poised for battle the panel positive and negative and carry out milling, (comprising chamfering) and two large each face of face stay 1mm allowance around the described front plate;
10) the front plate reaming after for the second time semifinishing
With in the middle of the front plate and periphery respectively organize aperture, counterbore and screwed hole bottom outlet and get out;
11) compacting of front plate is carried out heat treatment second time artificial aging at the special iron casting working plate, smoothing front plate after finishing guarantees flatness 0.15mm;
12) the front plate is carried out fine finishining, first around the processing, choose afterwards without the one side of counterbore and process under nature, then turn-over passes counterbore on the part with part compacting milling flat on working plate with screw, guarantees in size 12 ± 0.06 and the flatness 0.06mm;
13) the front plate after the fine finishining is carried out bore hole
Deburring after finishing, tapping;
14) get product after process on the surface of panel poised for battle.
2. the processing technology of the front plate of a front FRAME COMPONENTS claimed in claim 1, it is characterized in that: the working plate that described step 1) is used is cast iron plate.
3. the processing technology of the front plate of a front FRAME COMPONENTS claimed in claim 1 is characterized in that: described each Kong Kongwei is by the final size tolerance, guarantees that tolerance is in ± 0.05mm.
4. the processing technology of the front plate of a front FRAME COMPONENTS claimed in claim 1 is characterized in that: adopt the mode of Low Temperature Heat Treatment timeliness during described step 11) heat treatment timeliness, temperature is controlled at 180 ℃.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201210574441 CN103056615A (en) | 2013-02-04 | 2013-02-04 | Processing process of array panel of array face frame parts |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201210574441 CN103056615A (en) | 2013-02-04 | 2013-02-04 | Processing process of array panel of array face frame parts |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103056615A true CN103056615A (en) | 2013-04-24 |
Family
ID=48099658
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201210574441 Pending CN103056615A (en) | 2013-02-04 | 2013-02-04 | Processing process of array panel of array face frame parts |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103056615A (en) |
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105834698A (en) * | 2016-05-25 | 2016-08-10 | 江西洪都航空工业集团有限责任公司 | Milling method for solid solution steel hinge clamped by rotatable magnetic disk |
| CN104723021B (en) * | 2013-12-18 | 2017-04-05 | 中核建中核燃料元件有限公司 | Anti- foreign matter board machining process |
| CN107186437A (en) * | 2017-05-11 | 2017-09-22 | 江苏苏铃精工机械有限公司 | Three coordinate aluminium section bar processing technologys |
| CN108655672A (en) * | 2018-08-03 | 2018-10-16 | 杭州金浪机电有限公司 | A kind of integrally formed panel of cooker hood processing technology |
| CN108705268A (en) * | 2018-08-15 | 2018-10-26 | 江苏振江新能源装备股份有限公司 | Land wind-driven generator flange processing technology |
| CN108950440A (en) * | 2018-07-17 | 2018-12-07 | 苏州温锑姆精密机械有限公司 | Aluminium alloy plate processing technology |
| CN110170840A (en) * | 2019-06-05 | 2019-08-27 | 湖南凯斯机械股份有限公司 | A kind of processing method of baseplate of sewing machine and the processing unit (plant) of lower shaft hole and side shaft hole |
| CN110977330A (en) * | 2019-12-27 | 2020-04-10 | 东方电气(广州)重型机器有限公司 | Method for processing series holes of large-size thin-wall arched part |
| CN114083245A (en) * | 2021-12-17 | 2022-02-25 | 成都中电锦江信息产业有限公司 | Large array surface processing method based on virtual surface reference |
| CN114321181A (en) * | 2021-12-24 | 2022-04-12 | 徕司超精材料科技(苏州)有限公司 | Aluminum profile treatment process, aluminum profile and precision guide rail |
| CN114653996A (en) * | 2022-04-18 | 2022-06-24 | 广汽本田汽车有限公司 | Method for processing key structure workpiece of stamping die for automobile roof outer panel |
-
2013
- 2013-02-04 CN CN 201210574441 patent/CN103056615A/en active Pending
Cited By (15)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104723021B (en) * | 2013-12-18 | 2017-04-05 | 中核建中核燃料元件有限公司 | Anti- foreign matter board machining process |
| CN105834698A (en) * | 2016-05-25 | 2016-08-10 | 江西洪都航空工业集团有限责任公司 | Milling method for solid solution steel hinge clamped by rotatable magnetic disk |
| CN105834698B (en) * | 2016-05-25 | 2018-01-30 | 江西洪都航空工业集团有限责任公司 | A kind of solid solution steel hinge milling method using rotatable disc clamping |
| CN107186437A (en) * | 2017-05-11 | 2017-09-22 | 江苏苏铃精工机械有限公司 | Three coordinate aluminium section bar processing technologys |
| CN108950440A (en) * | 2018-07-17 | 2018-12-07 | 苏州温锑姆精密机械有限公司 | Aluminium alloy plate processing technology |
| CN108655672A (en) * | 2018-08-03 | 2018-10-16 | 杭州金浪机电有限公司 | A kind of integrally formed panel of cooker hood processing technology |
| CN108655672B (en) * | 2018-08-03 | 2019-10-25 | 杭州金浪机电有限公司 | A kind of integrally formed panel of cooker hood processing technology |
| CN108705268A (en) * | 2018-08-15 | 2018-10-26 | 江苏振江新能源装备股份有限公司 | Land wind-driven generator flange processing technology |
| CN108705268B (en) * | 2018-08-15 | 2020-05-19 | 江苏振江新能源装备股份有限公司 | Land wind driven generator flange machining process |
| CN110170840A (en) * | 2019-06-05 | 2019-08-27 | 湖南凯斯机械股份有限公司 | A kind of processing method of baseplate of sewing machine and the processing unit (plant) of lower shaft hole and side shaft hole |
| CN110977330A (en) * | 2019-12-27 | 2020-04-10 | 东方电气(广州)重型机器有限公司 | Method for processing series holes of large-size thin-wall arched part |
| CN114083245A (en) * | 2021-12-17 | 2022-02-25 | 成都中电锦江信息产业有限公司 | Large array surface processing method based on virtual surface reference |
| CN114321181A (en) * | 2021-12-24 | 2022-04-12 | 徕司超精材料科技(苏州)有限公司 | Aluminum profile treatment process, aluminum profile and precision guide rail |
| CN114653996A (en) * | 2022-04-18 | 2022-06-24 | 广汽本田汽车有限公司 | Method for processing key structure workpiece of stamping die for automobile roof outer panel |
| CN114653996B (en) * | 2022-04-18 | 2023-06-16 | 广汽本田汽车有限公司 | Machining method for key structural workpiece of automobile roof outer plate stamping die |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103056615A (en) | Processing process of array panel of array face frame parts | |
| CN103464996A (en) | Die production process | |
| CN207309468U (en) | A kind of milling tool of thin-walled parts | |
| CN103406725B (en) | A kind of flutter model roof beam structure processing method | |
| CN105562792A (en) | High-speed cutting method of thin-walled pod part | |
| CN103921068A (en) | Single-curvature cover machining method | |
| CN103007502A (en) | Manufacturing method for striking panel of golf club head | |
| CN106862456A (en) | Aluminum alloy mobile phone shell cold-heading stretch forming process | |
| CN204018675U (en) | The compression mod mold insert structure of edge spell shape formula and corresponding die casting | |
| CN105598635B (en) | A kind of fine structure part residual stress and machining deformation control method | |
| CN103397832B (en) | A kind of manufacture method of multi-frame door | |
| CN103834884B (en) | A kind ofly manufacture stamp work and eliminate method and the mould of unrelieved stress | |
| CN204308354U (en) | A kind of multi-cavity type electric machining graphite electrode | |
| CN105437426B (en) | A kind of reparation remodeling method of mould | |
| CN107009091B (en) | A kind of manufacturing method of metallic mobile phone shell | |
| CN204954397U (en) | Fragmentary external force clamping device of copper box of finish machining type communication work piece | |
| CN203779161U (en) | Flat square part milling tooling for roller shaft | |
| CN204221546U (en) | CNC machined burrs automatically removes magnetic grinder fast | |
| CN210254428U (en) | Floating deburring machine | |
| CN204546320U (en) | A kind of oilstone manufactures particular manufacturing craft | |
| CN206047623U (en) | A kind of fluting plug screw Full automatic groover | |
| CN205415212U (en) | Two -sided strengthening rib angle molding device | |
| CN104646687A (en) | Aluminum piston machining method | |
| CN203649443U (en) | Boring lathe cutter holder | |
| CN103817503A (en) | Mold sprue production method |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20130424 |