CN105382560A - Control plane body milling tool - Google Patents
Control plane body milling tool Download PDFInfo
- Publication number
- CN105382560A CN105382560A CN201410443202.3A CN201410443202A CN105382560A CN 105382560 A CN105382560 A CN 105382560A CN 201410443202 A CN201410443202 A CN 201410443202A CN 105382560 A CN105382560 A CN 105382560A
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- China
- Prior art keywords
- base plate
- screws
- control plane
- plane body
- body milling
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- 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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Abstract
Provided is a control plane body milling tool, relating to a milling tool. The invention especially relates to the control plane body milling tool for the purpose of solving problems that a middle groove and a left inclined edge of a milled control plane body part are hard to clamp; efficiency is low, and part machining precision cannot be ensured. The control plane body milling tool comprises a bottom plate, two pressing plates and four M10 hexagon socket screws. The bottom plate is a rectangular and is horizontally arranged. A rectangular groove is formed in the middle of the upper surface of the bottom plate. A circular bead is arranged on one side in the rectangular groove. The size of the circular bead of the rectangular groove is matched with the relevant size of the part. Two first screw holes are formed in one side of the upper surface of the bottom plate in the length direction, two second screw holes are formed in the rectangular groove in the length direction. Two mounting gaps are formed in each side edge of the bottom plate. The two pressing plates are arranged in the two first screw holes through two M10 hexagon socket screws, and workpieces are arranged in the two second screw holes through the other two M10 hexagon socket screws. The control plane body milling tool is used for machining the control plane body workpieces.
Description
Technical field
The present invention relates to a kind of milling type frock, be specifically related to a kind of rudder face body milling type frock, belong to field of machining.
Background technology
Existing rudder face body part work in-process, adopt the mode of low-speed WEDM to process middle groove and left side hypotenuse, long processing time, processing cost is high; In order to reduce costs, therefore adopt the method for Milling Process to process two positions, place, but clamping is difficult, efficiency is lower, and the machining accuracy of part is also difficult to ensure.
Summary of the invention
The present invention is for solving Milling Process rudder face body part medial launder and left side hypotenuse clamping difficulty, and efficiency is low, and part processing precision is difficult to the problem of guarantee, and then design rudder face body milling type frock.
The present invention is the technical scheme taked that solves the problem: the present invention includes base plate, two pressing plates and four M10 hexagon socket head cap screws, base plate is rectangle plate body, floor level is arranged, the middle part of plate upper surface has rectangular recess, side in rectangular recess is provided with shoulder, its shoulder size conforms to part relative dimensions, the side of plate upper surface is provided with two the first screws along its length, rectangular recess is provided with two the second screws along its length, each lateral edges of base plate all has two and installs gap, two pressing plates are arranged in two the first screws by two M10 hexagon socket head cap screws, workpiece is arranged in two the second screws by two M10 hexagon socket head cap screws.
The invention has the beneficial effects as follows: the production efficiency that invention increases work pieces process, reduce cost, solve the processing limitation that Workpiece structure causes, more easily adapt to production and processing, the present invention includes the accurate location to workpiece, for the processing characteristic of aluminum alloy material variable inclination class part, the required precision of part itself is utilized to position, 2 place's pressing plates are adopted mainly to clamp, the mode of 2 place's bolt auxiliary clamps, reliable clamping force and positioning precision are provided, in addition, adopt less cutter, rational cutting parameter, make every effort to that cutting force is minimum to be processed, the present invention accurately locates workpiece, and workpiece all need not carry out centering at every turn and zero point is processed in check and correction, thus reduces the labour intensity of staff, improves working (machining) efficiency, the present invention adopts rational location, clamping, has widened the processing limitation of part, has reduced processing cost, improve production efficiency.
Accompanying drawing explanation
Fig. 1 is overall structure schematic diagram of the present invention, and Fig. 2 is that in Fig. 1, A-A is to sectional view, and Fig. 3 is the top view of base plate.
Detailed description of the invention
Detailed description of the invention one: composition graphs 1 to Fig. 3 illustrates present embodiment, described in present embodiment, a kind of rudder face body milling type frock comprises base plate 1, two pressing plates 4 and four M10 hexagon socket head cap screws 3, base plate 1 is rectangle plate body, base plate 1 is horizontally disposed with, the middle part of base plate 1 upper surface has rectangular recess 1-1, side in rectangular recess 1-1 is provided with shoulder 1-2, the side of base plate 1 upper surface is provided with two the first screw 1-3 along its length, rectangular recess 1-1 is provided with two the second screw 1-4 along its length, each lateral edges of base plate 1 all has two and installs gap 1-5, two pressing plates 4 are arranged in two the first screw 1-3 by two M10 hexagon socket head cap screws 3, workpiece 5 is arranged in two the second screw 1-4 by two M10 hexagon socket head cap screws 3.
Detailed description of the invention two: composition graphs 1 to Fig. 3 illustrates present embodiment, described in present embodiment, a kind of rudder face body milling type frock also comprises two cushion blocks 2, is respectively provided with a cushion block 2 respectively between the lower surface of each pressing plate 4 and the upper surface of base 1.
The technique effect of present embodiment is: so arrange, other composition and annexation identical with detailed description of the invention one.
Detailed description of the invention three: composition graphs 1 to Fig. 3 illustrates present embodiment, described in present embodiment, a kind of length of base plate 1 of rudder face body milling type frock is 340mm, and the width of base plate 1 is 240mm, and the thickness of base plate 1 is 30mm.Other composition and annexation identical with detailed description of the invention one or two.
Detailed description of the invention four: composition graphs 1 to Fig. 3 illustrates present embodiment, described in present embodiment, the height of a kind of shoulder 1-2 of rudder face body milling type frock is 3mm, centre-to-centre spacing between two the first screw 1-3 is 140mm, centre-to-centre spacing between two the second screw 1-4 is 140mm, two centre-to-centre spacing of installing gap 1-5 being positioned at the same side are 240mm, and the width of each gap 1-5 is 20mm.Other composition and annexation identical with detailed description of the invention three.
Claims (4)
1. a rudder face body milling type frock, it is characterized in that: described a kind of rudder face body milling type frock comprises base plate (1), two pressing plates (4) and four M10 hexagon socket head cap screws (3), base plate (1) is rectangle plate body, base plate (1) is horizontally disposed with, the middle part of base plate (1) upper surface has rectangular recess (1-1), side in rectangular recess (1-1) is provided with shoulder (1-2), the side of base plate (1) upper surface is provided with two the first screws (1-3) along its length, rectangular recess (1-1) is provided with two the second screws (1-4) along its length, base plate (1) each lateral edges all has two and installs gap (1-5), two pressing plates (4) are arranged in two the first screws (1-3) by two M10 hexagon socket head cap screws (3), workpiece (5) is arranged in two the second screws (1-4) by two M10 hexagon socket head cap screws (3).
2. a kind of rudder face body milling type frock according to claim 1, it is characterized in that: described a kind of rudder face body milling type frock also comprises two cushion blocks (2), is respectively provided with a cushion block (2) between the lower surface of each pressing plate (4) and the upper surface of base (1) respectively.
3. a kind of rudder face body milling type frock according to claim 1 or 2, it is characterized in that: the length of base plate (1) is 340mm, the width of base plate (1) is 240mm, and the thickness of base plate (1) is 30mm.
4. a kind of rudder face body milling type frock according to claim 3, it is characterized in that: the height of shoulder (1-2) is 3mm, centre-to-centre spacing between two the first screws (1-3) is 140mm, centre-to-centre spacing between two the second screws (1-4) is 140mm, two centre-to-centre spacing of installing gap (1-5) being positioned at the same side are 240mm, and the width of each gap (1-5) is 20mm.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410443202.3A CN105382560A (en) | 2014-09-03 | 2014-09-03 | Control plane body milling tool |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410443202.3A CN105382560A (en) | 2014-09-03 | 2014-09-03 | Control plane body milling tool |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105382560A true CN105382560A (en) | 2016-03-09 |
Family
ID=55415683
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410443202.3A Pending CN105382560A (en) | 2014-09-03 | 2014-09-03 | Control plane body milling tool |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105382560A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106271740A (en) * | 2016-08-30 | 2017-01-04 | 北京零壹空间科技有限公司 | The processing tool of rudder and processing method |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201016896Y (en) * | 2007-03-27 | 2008-02-06 | 宝山钢铁股份有限公司 | Clamping device for milling sample piece |
| CN201089092Y (en) * | 2007-10-31 | 2008-07-23 | 天津市天发重型水电设备制造有限公司 | Multipurpose assembly for stop-pad drilling |
| CN201442176U (en) * | 2009-07-20 | 2010-04-28 | 莱芜钢铁集团有限公司 | Expanded work bench for machine tool |
| GB2476988A (en) * | 2010-01-19 | 2011-07-20 | Alfred Hamer | Work piece-holding jig for a lathe |
| CN203509678U (en) * | 2013-10-28 | 2014-04-02 | 哈尔滨汽轮机厂有限责任公司 | Milling blade root middle body in and out steam side clamp used clamp |
| CN203664761U (en) * | 2013-12-19 | 2014-06-25 | 中航贵州飞机有限责任公司 | Open type general positioning device |
| CN204053540U (en) * | 2014-09-03 | 2014-12-31 | 哈尔滨建成集团有限公司 | A kind of rudder face body milling type frock |
-
2014
- 2014-09-03 CN CN201410443202.3A patent/CN105382560A/en active Pending
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201016896Y (en) * | 2007-03-27 | 2008-02-06 | 宝山钢铁股份有限公司 | Clamping device for milling sample piece |
| CN201089092Y (en) * | 2007-10-31 | 2008-07-23 | 天津市天发重型水电设备制造有限公司 | Multipurpose assembly for stop-pad drilling |
| CN201442176U (en) * | 2009-07-20 | 2010-04-28 | 莱芜钢铁集团有限公司 | Expanded work bench for machine tool |
| GB2476988A (en) * | 2010-01-19 | 2011-07-20 | Alfred Hamer | Work piece-holding jig for a lathe |
| CN203509678U (en) * | 2013-10-28 | 2014-04-02 | 哈尔滨汽轮机厂有限责任公司 | Milling blade root middle body in and out steam side clamp used clamp |
| CN203664761U (en) * | 2013-12-19 | 2014-06-25 | 中航贵州飞机有限责任公司 | Open type general positioning device |
| CN204053540U (en) * | 2014-09-03 | 2014-12-31 | 哈尔滨建成集团有限公司 | A kind of rudder face body milling type frock |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106271740A (en) * | 2016-08-30 | 2017-01-04 | 北京零壹空间科技有限公司 | The processing tool of rudder and processing method |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
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| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20160309 |
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| WD01 | Invention patent application deemed withdrawn after publication |