CN106583786A - Manufacturing method of molding frame with space angle positioning hole and molding frame manufactured thereby - Google Patents
Manufacturing method of molding frame with space angle positioning hole and molding frame manufactured thereby Download PDFInfo
- Publication number
- CN106583786A CN106583786A CN201611115913.3A CN201611115913A CN106583786A CN 106583786 A CN106583786 A CN 106583786A CN 201611115913 A CN201611115913 A CN 201611115913A CN 106583786 A CN106583786 A CN 106583786A
- Authority
- CN
- China
- Prior art keywords
- space angle
- type frame
- hole
- clamp
- location hole
- 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.)
- Granted
Links
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 30
- 238000000465 moulding Methods 0.000 title abstract 6
- 238000000034 method Methods 0.000 claims description 21
- 239000011159 matrix material Substances 0.000 claims description 19
- 238000004088 simulation Methods 0.000 claims description 19
- 238000009434 installation Methods 0.000 claims description 6
- 239000004568 cement Substances 0.000 claims description 4
- 230000008676 import Effects 0.000 claims description 4
- 239000011111 cardboard Substances 0.000 claims description 2
- 238000003754 machining Methods 0.000 abstract description 6
- 230000008569 process Effects 0.000 description 4
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008859 change Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 238000011946 reduction process Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23B—TURNING; BORING
- B23B41/00—Boring or drilling machines or devices specially adapted for particular work; Accessories specially adapted therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23Q—DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
- B23Q15/00—Automatic control or regulation of feed movement, cutting velocity or position of tool or work
- B23Q15/20—Automatic control or regulation of feed movement, cutting velocity or position of tool or work before or after the tool acts upon the workpiece
- B23Q15/22—Control or regulation of position of tool or workpiece
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23Q—DETAILS, COMPONENTS, OR ACCESSORIES FOR MACHINE TOOLS, e.g. ARRANGEMENTS FOR COPYING OR CONTROLLING; MACHINE TOOLS IN GENERAL CHARACTERISED BY THE CONSTRUCTION OF PARTICULAR DETAILS OR COMPONENTS; COMBINATIONS OR ASSOCIATIONS OF METAL-WORKING MACHINES, NOT DIRECTED TO A PARTICULAR RESULT
- B23Q17/00—Arrangements for observing, indicating or measuring on machine tools
- B23Q17/24—Arrangements for observing, indicating or measuring on machine tools using optics or electromagnetic waves
- B23Q17/2428—Arrangements for observing, indicating or measuring on machine tools using optics or electromagnetic waves for measuring existing positions of tools or workpieces
Abstract
The invention discloses a manufacturing method of a molding frame with a space angle positioning hole. The manufacturing method comprises the steps of: manufacturing of analog reference holes, manufacturing of the space angle positioning hole, manufacturing of reference holes, accurate positioning adjustment of the space angle positioning hole by a laser tracking instrument, and mounting of a clamping plate or a positioning plate with a molding frame basal body; and the manufacturing of the analog reference hole is finished in a three-dimensional digital model. The invention further discloses the molding frame with the space angle positioning hole and manufactured by the manufacturing method. The manufacturing method of the molding frame with the space angle positioning hole can reduce the machining cost and the machining operation difficulty, and facilitates machining and popularization of the space angle positioning hole.
Description
Technical field
The present invention relates to machining and mould, type frame manufacture field, and in particular to a kind of carrying space angle positions pass
The manufacture method of frame and the type frame made by the method.
Background technology
The major part of positioning or orientation from frequently encountering in machining when some are assembled, these parts are often
Location hole with space angle needs to carry out polish, but the precision in the angled hole of three axis numerically controlled machine processing of routine is
It is difficult to ensure that.
In the processing with space angle pass frame, general three axis numerically controlled machine is difficult to, therefore many using high-grade
Lathe, is such as punched using 5-shaft linkage numerical control lathe in overall type frame, realizes the location and installation of type frame.But general five axles connection
Dynamic Digit Control Machine Tool is expensive, and processing charges is high and is only limitted to process small-sized type frame, if large-scale type frame is installed in processing, then
Large-scale five-axis machine tool must be customized；Simultaneously in overall type frame punching there are problems that difficulty is big, precision not；This
Outward, punch in overall type frame, type frame clamp or location-plate need to meet corresponding thickness requirement, if thickness low LCL, can produce
Life is substantial amounts of to scrap unit.
The content of the invention
Present invention aim to address above-mentioned problems of the prior art and a kind of carrying space angle location hole is provided
The manufacture method of type frame, it is possible to reduce processing cost, reduction process operation difficulty, the processing for being conducive to space angle location hole is pushed away
Extensively.
The purpose of the present invention is achieved through the following technical solutions：
A kind of manufacture method of carrying space angle location hole type frame, it includes following operation：
（1）The making of simulation datum hole
In three-dimensional digital-to-analogue, simulation datum hole is produced on simulation clamp and simulation type frame matrix respectively；
（2）The making of space angle location hole
According to step（1）Middle three-dimensional digital-to-analogue to simulating the relative position dimensional requirement of space angle location hole, using right boring or
Three axis numerically controlled machine manufacturing procedure, produces space angle location hole on clamp；
（3）The making of datum hole
According to step（1）Relative position dimensional requirement of the middle three-dimensional digital-to-analogue to simulation datum hole, respectively in clamp and type frame matrix
On produce datum hole；
（4）The positioning of space angle location hole
By step（1）In three-dimensional digital-to-analogue import laser tracker, find the datum hole on type frame matrix accurately using target ball, it is determined that swash
The coordinate system of three-dimensional digital-to-analogue in optical tracker system；
Target ball is placed at clamp datum hole, clamp position is adjusted, clamp position is simulated in three-dimensional digital-to-analogue in contrast laser tracker
The related data with actual card Board position and size is put, clamp position is adjusted again, until both data difference is ± 0.01mm's
In the margin of tolerance；
（5）The making of type frame
According to step（4）The positioning of middle laser tracker is adjusted, and in clamp relevant position threaded connection hole and top wire hole are produced,
Corresponding threaded connection hole and top wire hole are made on type frame matrix, clamp and type frame matrix are connected to into one by securing member
Rise, with quick hardening cement clamp is fixed, complete clamp installation, it is final to make the type frame for obtaining carrying space angle location hole.
Preferably, the clamp is replaced with location-plate.
Preferably, the relative position dimensional tolerance of the space angle location hole is ± 0.05mm.
Preferably, the securing member is screw or bolt.
It is a further object of the present invention to provide a kind of type frame with space angle location hole, it is by above-mentioned making step system
Obtain.
The present invention has following beneficial effect：
Individually corresponding clamp or location-plate are punched using right boring or three axle machine tooling operations, face, Dan Jiao can be tied
Degree hole or double angle hole, then installation clamp or location-plate are accurately positioned with laser tracker, solve in common process with five
Shaft and NC Machining Test linkage machine tool directly punches to the clamp in overall type frame or location-plate, and the difficulty for existing is big, precision is not up to standard, processing
It is costly, customize large-scale five-axis machine tool the problems such as；The method of the present invention is not required clamp or positioning plate thickness, solved
To the problem of type frame clamp thickness requirement in conventional processes, in can be applied not only to the making of small-sized type frame or mould, may be used also
In to be applied to the making of large-scale type frame or mould.
Specific embodiment
With reference to specific embodiment, the present invention will be further explained.It should be noted that the present invention
The manufacture method of carrying space angle location hole type frame and should not be limited to be enumerated in example below by its type frame product for making
Situation, those skilled in the art in the case where any creative work is not made, the present invention is done any flexible and
Change, it is believed that falling within the scope of the present invention.
Embodiment 1
The required precision of space angle location hole in the present embodiment is H8, the relative position dimensional tolerance of two location holes for ±
0.05mm, processing and fabricating for large-scale type frame, its manufacture method includes following operation：
（1）The making of simulation datum hole
In three-dimensional digital-to-analogue, 2 simulation datum hole φ 5H8 are produced respectively on simulation clamp and simulation type frame matrix；
（2）The making of space angle location hole
According to step（1）Middle three-dimensional digital-to-analogue to simulating the relative position dimensional requirement of space angle location hole, using right boring or
Three axis numerically controlled machine manufacturing procedure, produces the space angle location hole of 4 φ 8H8 on clamp；
（3）The making of datum hole
According to step（1）Relative position dimensional requirement of the middle three-dimensional digital-to-analogue to simulation datum hole, in clamp and the phase of type frame matrix
Position is answered to produce the datum hole of 2 φ 5H8 respectively；
（4）The positioning of space angle location hole
By step（1）In three-dimensional digital-to-analogue import laser tracker, find the datum hole of φ 5H8 on type frame matrix accurately using target ball,
Determine the coordinate system of three-dimensional digital-to-analogue in laser tracker；
Target ball is placed at clamp datum hole, clamp position is adjusted, is contrasted in three-dimensional digital-to-analogue using laser tracker and is simulated clamp
Position and the related data of clamp position dimension in practice, adjust again clamp position, until both data difference is in ± 0.01mm
The margin of tolerance in；
（5）The making of type frame
According to step（4）The positioning of middle laser tracker is adjusted, and in clamp relevant position threaded connection hole and top wire hole are produced,
Corresponding threaded connection hole and top wire hole are made on type frame matrix, clamp is connected by screw with type frame matrix together with,
Clamp is fixed with quick hardening cement, clamp installation is completed, the large-scale type frame of carrying space angle location hole is finally given.
Embodiment 2
The required precision of space angle location hole in the present embodiment is H8, the relative position dimensional tolerance of two location holes for ±
0.05mm, processing and fabricating for frock weld jig, belong to small-sized type frame, its manufacture method includes following operation：
（1）The making of simulation datum hole
In three-dimensional digital-to-analogue, 2 simulation datum hole φ are produced respectively on simulator locating plate and simulation weld jig matrix
5H8；
（2）The making of space angle location hole
According to step（1）Middle three-dimensional digital-to-analogue to simulating the relative position dimensional requirement of space angle location hole, using right boring or
Three axis numerically controlled machine manufacturing procedure, produces the space angle location hole of 4 φ 3H8 on location-plate；
（3）The making of datum hole
According to step（1）Relative position dimensional requirement of the middle three-dimensional digital-to-analogue to simulation datum hole, in location-plate and weld jig base
The datum hole of 2 φ 5H8 is produced respectively in the relevant position of body；
（4）The positioning of space angle location hole
By step（1）In three-dimensional digital-to-analogue import laser tracker, find the benchmark of φ 5H8 on weld jig matrix accurately using target ball
Hole, determines the coordinate system of three-dimensional digital-to-analogue in laser tracker；
Target ball is placed at location-plate datum hole, positioning Board position is adjusted, is contrasted using laser tracker and is simulated in three-dimensional digital-to-analogue
Positioning Board position and the related data of location-plate position dimension in practice, adjust again positioning Board position, until both data is poor
In the margin of tolerance of ± 0.01mm；
（5）The making of weld jig
According to step（4）The positioning of middle laser tracker is adjusted, and in location-plate relevant position threaded connection hole and jackscrew are produced
Hole, makes corresponding threaded connection hole and top wire hole on weld jig matrix, and location-plate and weld jig matrix are passed through into spiral shell
Nail links together, and with quick hardening cement location-plate is fixed, and completes location-plate installation, and final making obtains carrying space angle positioning
The weld jig in hole, that is, make and obtain small-sized type frame.
The manufacture method of the carrying space angle location hole type frame in the present invention, when without five-shaft numerical control linkage machine tool,
Can make of common three axis numerically controlled machine and obtain, required required precision not only can be reached, and solve five number of axle
The control operation difficulty that has of linkage machine tool is big, production cost is high, high to type frame clamp or location-plate thickness requirement and large-scale type
Frame needs the problem for customizing five-axis machine tool；Have the advantages that low expense, high precision, accuracy are high, easy to process, not only can answer
In making for small-sized type frame or mould, it is also possible in being applied to the making of large-scale type frame or mould.
Claims (6)
1. a kind of manufacture method of carrying space angle location hole type frame, it is characterised in that it includes following operation：
（1）The making of simulation datum hole
In three-dimensional digital-to-analogue, simulation datum hole is produced on simulation clamp and simulation type frame matrix respectively；
（2）The making of space angle location hole
According to step（1）Middle three-dimensional digital-to-analogue to simulating the relative position dimensional requirement of space angle location hole, using right boring or
Three axis numerically controlled machine manufacturing procedure, produces space angle location hole on clamp；
（3）The making of datum hole
According to step（1）Relative position dimensional requirement of the middle three-dimensional digital-to-analogue to simulation datum hole, respectively in clamp and type frame matrix
On produce datum hole；
（4）The positioning of space angle location hole
By step（1）In three-dimensional digital-to-analogue import laser tracker, it is accurately fixed to space angle location hole using laser tracker
Position；
（5）The making of type frame
According to step（4）The positioning of middle laser tracker is adjusted, and in clamp relevant position threaded connection hole and top wire hole are produced,
Corresponding threaded connection hole and top wire hole are made on type frame matrix, clamp and type frame matrix are connected to into one by securing member
Rise, with quick hardening cement clamp is fixed, complete clamp installation, making obtains the type frame of carrying space angle location hole.
2. the manufacture method of carrying space angle location hole type frame according to claim 1, it is characterised in that：The step
（4）In, the positioning step of space angle location hole is as follows：
The datum hole on type frame matrix is found accurately using target ball, determine three-dimensional digital-to-analogue coordinate system in laser tracker；
Target ball is placed at clamp datum hole, clamp position is adjusted, is contrasted in three-dimensional digital-to-analogue using laser tracker and is simulated clamp
Position and the related data of actual card Board position size, adjust again clamp position, until both data difference is ± 0.01mm's
In the margin of tolerance.
3. the manufacture method of carrying space angle location hole type frame according to claim 1, it is characterised in that：Use location-plate generation
For clamp.
4. the manufacture method of carrying space angle location hole type frame according to claim 1, it is characterised in that：The Space Angle
The relative position dimensional tolerance of degree location hole is ± 0.05mm.
5. the manufacture method of carrying space angle location hole type frame according to claim 1, it is characterised in that：The securing member
For screw or bolt.
6. the type frame that a kind of manufacture method by described in any one of claim 1-5 makes, it is characterised in that：The type frame be by
The type frame with space angle location hole that above-mentioned manufacture method is prepared.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611115913.3A CN106583786B (en) | 2016-12-07 | 2016-12-07 | A kind of production method of carrying space angle location hole type frame and the type frame by its making |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611115913.3A CN106583786B (en) | 2016-12-07 | 2016-12-07 | A kind of production method of carrying space angle location hole type frame and the type frame by its making |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106583786A true CN106583786A (en) | 2017-04-26 |
| CN106583786B CN106583786B (en) | 2018-05-08 |
Family
ID=58597313
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611115913.3A Expired - Fee Related CN106583786B (en) | 2016-12-07 | 2016-12-07 | A kind of production method of carrying space angle location hole type frame and the type frame by its making |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106583786B (en) |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2004261924A (en) * | 2003-03-03 | 2004-09-24 | Seiko Precision Inc | Boring device for plate-like work and boring method |
| CN101776440A (en) * | 2010-02-03 | 2010-07-14 | 北京航空航天大学 | Method for assembling and locating web-type wing ribs on basis of laser measurement |
| JP2012190113A (en) * | 2011-03-09 | 2012-10-04 | Toyota Central R&D Labs Inc | Processing data generation system, and solver program |
| CN103418815A (en) * | 2013-08-06 | 2013-12-04 | 中铁建钢结构有限公司 | Box-type steel member bolting hole group axial positioning method |
| CN103759646A (en) * | 2014-01-27 | 2014-04-30 | 哈尔滨飞机工业集团有限责任公司 | Method for locating and installing locating piece through threaded hole |
| CN103955168A (en) * | 2014-04-22 | 2014-07-30 | 浙江大学 | Robot hole machining off-line programming method based on DELMIA simulation |
| CN205702547U (en) * | 2016-06-24 | 2016-11-23 | 微山县兴玉机械制造有限公司 | A kind of boring equipment taking turns limit planet carrier |
-
2016
- 2016-12-07 CN CN201611115913.3A patent/CN106583786B/en not_active Expired - Fee Related
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2004261924A (en) * | 2003-03-03 | 2004-09-24 | Seiko Precision Inc | Boring device for plate-like work and boring method |
| CN101776440A (en) * | 2010-02-03 | 2010-07-14 | 北京航空航天大学 | Method for assembling and locating web-type wing ribs on basis of laser measurement |
| JP2012190113A (en) * | 2011-03-09 | 2012-10-04 | Toyota Central R&D Labs Inc | Processing data generation system, and solver program |
| CN103418815A (en) * | 2013-08-06 | 2013-12-04 | 中铁建钢结构有限公司 | Box-type steel member bolting hole group axial positioning method |
| CN103759646A (en) * | 2014-01-27 | 2014-04-30 | 哈尔滨飞机工业集团有限责任公司 | Method for locating and installing locating piece through threaded hole |
| CN103955168A (en) * | 2014-04-22 | 2014-07-30 | 浙江大学 | Robot hole machining off-line programming method based on DELMIA simulation |
| CN205702547U (en) * | 2016-06-24 | 2016-11-23 | 微山县兴玉机械制造有限公司 | A kind of boring equipment taking turns limit planet carrier |
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| Publication number | Publication date |
|---|---|
| CN106583786B (en) | 2018-05-08 |
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| TR01 | Transfer of patent right |
Effective date of registration: 20190201 Address after: 051430 No. 99 Hengjing Road, Luancheng District, Shijiazhuang City, Hebei Province Patentee after: SHIJIAZHUANG ZHONGHANG MECHANICAL AND ELECTRICAL EQUIPMENT MANUFACTURING Co.,Ltd. Address before: 051430 No. 99 Hengjing Road, Shijiazhuang City, Hebei Province Patentee before: AVIC SHIJIAZHUANG AIRCRAFT INDUSTRY (GROUP) Corp.,Ltd. |
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Granted publication date: 20180508 |
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