CN203955990U - Connect aerofoil profile saddle bracket forge die - Google Patents
Connect aerofoil profile saddle bracket forge die Download PDFInfo
- Publication number
- CN203955990U CN203955990U CN201420389339.0U CN201420389339U CN203955990U CN 203955990 U CN203955990 U CN 203955990U CN 201420389339 U CN201420389339 U CN 201420389339U CN 203955990 U CN203955990 U CN 203955990U
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- China
- Prior art keywords
- saddle bracket
- projection
- overflow
- stops
- die
- 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.)
- Expired - Lifetime
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- 229910000831 Steel Inorganic materials 0.000 claims description 6
- 239000010959 steel Substances 0.000 claims description 6
- 239000000463 material Substances 0.000 claims description 5
- 238000003825 pressing Methods 0.000 claims description 5
- 238000005242 forging Methods 0.000 abstract description 18
- 238000004519 manufacturing process Methods 0.000 abstract description 8
- 230000000903 blocking effect Effects 0.000 abstract description 6
- 238000005516 engineering process Methods 0.000 abstract description 4
- 238000007723 die pressing method Methods 0.000 abstract 1
- 238000003801 milling Methods 0.000 description 5
- 238000010438 heat treatment Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- 238000001816 cooling Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 238000000465 moulding Methods 0.000 description 2
- 238000009966 trimming Methods 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000010892 electric spark Methods 0.000 description 1
- 238000005265 energy consumption Methods 0.000 description 1
- 238000000227 grinding Methods 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 238000005496 tempering Methods 0.000 description 1
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- Forging (AREA)
Abstract
The utility model discloses a kind of aerofoil profile saddle bracket forge die that connects, it relates to saddle bracket manufacturing technology field, it comprises upper die and lower die, patrix has the upper impression identical with the upper profile shape of saddle bracket, counterdie has the lower impressions identical with the lower profile shape of saddle bracket, the edge of upper impression and lower impressions is all surrounded with stitching surface, upper die and lower die all have the overflow launder for holding clout, counterdie has four overflows and stops projection, overflow stops that projection is positioned at four angle positions that connecting wing and saddle bracket main body are, patrix has with overflow and stops the groove that projection matches, when upper die and lower die pressing, overflow stops between projection and groove to have gap.It is for connecting the forging and stamping manufacture of aerofoil profile saddle bracket, and especially connecting wing is full complete can to ensure to forge and press the each several part of rear saddle bracket, thereby saves blocking operation, saves blank, enhances productivity.
Description
Technical field
The utility model relates to saddle bracket manufacturing technology field.
Background technology
Saddle bracket is a vitals in Messenger Wire base, and it plays the effect of direct carrying carrier cable.National standard " parts of electrified railway contact network " is described to some extent to the structure of Messenger Wire base in (TB/T2075-2010), for single groove Messenger Wire base, the main body of its saddle bracket is a saddle-shaped line holder, respectively there is a leg-of-mutton connecting wing both sides of line holder, there is a circular hole running through from top to bottom at Xian Tuo center, respectively has a connecting hole in connecting wing.When use, line ball clamping plate, carrier cable, saddle bracket, Messenger Wire base body stacked successively and fix with bolt, wherein carrier cable passes through from saddle-shaped line holder just.
Under prior art, the production that connects aerofoil profile saddle bracket is to adopt mould forging and stamping to manufacture, before forging and stamping, first calculate the specification of blank used according to the drawing of saddle type bearing, then by blank heating, put it into again in special mould, forge and press with forging press, thereby obtain the forging and stamping blank of saddle type bearing.
Because blank generally adopts cylinder blank, and the tip portion of connecting wing is thinner and far away apart from center, therefore while forging and stamping, often produce the incomplete phenomenon of the most advanced and sophisticated moulding of connecting wing, in order to address this problem, conventionally before formal forging and stamping, increase blocking operation one, blocking is to adopt larger cylinder blank, and extrude a winglet extending to both sides in the centre of this blank, owing to having increased by a procedure, and blank consumption increases, just make whole production process become comparatively complicated, energy consumption is also large, forging cost increases, simultaneously, owing to having increased prefabricated blank operation, in whole production process, just need to repeatedly suppress the blank after heating, thereby cause the sharply decline of blank temperature, this has also affected the final performance of part.
Utility model content
The technical problems to be solved in the utility model is for above-mentioned the deficiencies in the prior art, a kind of aerofoil profile saddle bracket forge die that connects is provided, it can make blank flow to the position of needs, the main body and the connecting wing that ensure the rear saddle bracket of forging and stamping are all full complete, thereby save blocking operation, save blank, enhance productivity.
For solving the problems of the technologies described above, technical solution adopted in the utility model is: a kind of aerofoil profile saddle bracket forge die that connects, it comprises upper die and lower die, patrix has the upper impression identical with the upper profile shape of saddle bracket, counterdie has the lower impressions identical with the lower profile shape of saddle bracket, the edge of upper impression and lower impressions is all surrounded with stitching surface, patrix stitching surface is identical with the shape of counterdie stitching surface, when compressing, upper and lower mould has the gap of flowing out for clout between patrix stitching surface and counterdie stitching surface, upper die and lower die also have the overflow launder for holding clout, overflow launder is looped around outside stitching surface, counterdie has four overflows and stops projection, overflow stops that projection is positioned at four angle positions that connecting wing and saddle bracket main body are, these four overflows stop that projection can limit blank from the both sides of connecting wing and flow out the both sides of saddle bracket main body, make blank to the tip of connecting wing and the two ends of saddle bracket main body flow, ensure that these four position moulding are complete full, patrix has with overflow and stops the groove that projection matches, when upper and lower mould pressing, overflow stops between projection and groove to have gap.
As preferably, overflow stops that projection is between overflow launder and stitching surface.
As preferably, when upper and lower mould pressing, overflow stops between the side of projection and end face and groove all have the gap of 2 millimeters, and when forging and stamping, unnecessary blank can flow out from this gap.
As preferably, four jiaos of counterdie have guide pad, and four jiaos of patrix have the guide pad groove suitable with guide pad, and guide pad and guide pad groove limit the relative position of upper and lower mould jointly, ensure that both can not misplace.
As preferably, overflow stops that projection is four prism type, and its length is 15～40 millimeters, and width is 10～30 millimeters, is highly 6～20 millimeters.
As preferably, the material of upper die and lower die is H13 steel (H13 steel is the hot die steel that in GB/T1299-2000 standard, the trade mark is 4Cr5MoSiV1).
The beneficial effect that adopts technique scheme to produce is: the utility model adds overflow to stop projection in mould, can limit whens forging and stamping blank from connecting wing both sides and the both sides of saddle bracket main body flow out, thereby make blank to the tip of connecting wing and the two end portions of saddle bracket main body flow, after guarantee forging and stamping, especially connecting wing is full complete for the each several part of saddle bracket, save blocking operation, save blank, enhance productivity, very practical.
Brief description of the drawings
Fig. 1 is the lower die structure schematic diagram of embodiment 1;
Fig. 2 is the partial enlarged drawing of Fig. 1;
Fig. 3 is the upper die structure schematic diagram of embodiment 1;
Fig. 4 is the structural representation that connects aerofoil profile saddle bracket.
In figure: 1, overflow stops projection; 2, lower impressions; 3, guide pad; 4, stitching surface; 5, overflow launder; 6, upper impression; 7, guide pad groove; 8, groove; 9, connecting wing.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the utility model is described in further detail.
Embodiment 1:
As Fig. 1, 2, 3, shown in 4, a kind of forge die of the saddle bracket with connecting wing, it comprises upper die and lower die, patrix has the upper impression 6 identical with the upper profile shape of saddle bracket, counterdie has the lower impressions 2 identical with the lower profile shape of saddle bracket, the edge of upper impression 6 and lower impressions 2 is all surrounded with stitching surface 4, patrix stitching surface is identical with the shape of counterdie stitching surface, when compressing, upper and lower mould has the gap of flowing out for clout between patrix stitching surface and counterdie stitching surface, upper die and lower die all have the overflow launder 5 for holding clout, overflow launder 5 is looped around outside stitching surface 4, four jiaos of counterdie have guide pad 3, four jiaos of patrix have the guide pad groove 7 suitable with guide pad, counterdie has four prism type overflow and stops projection 1, its length is 20 millimeters, width is 15 millimeters, be highly 13 millimeters, overflow stops that projection 1 has four, lay respectively at four angle positions that connecting wing 9 and saddle bracket main body are, and on the position between overflow launder 5 and stitching surface 4, patrix also has with overflow and stops the groove 8 that projection 1 matches, overflow stops between the side of projection 1 and end face and groove 8 all have 2 millimeters of gaps, blank can flow out from this gap.
Embodiment 2:
Identical with embodiment 1, just four prism type overflow stops that the length of projection 1 is 15 millimeters, and width is 10 millimeters, is highly 6 millimeters.
Embodiment 3:
Identical with embodiment 1, just four prism type overflow stops that the length of projection 1 is 40 millimeters, and width is 30 millimeters, is highly 20 millimeters.
The material of this mould is H13 steel, its parameter is followed the requirement of the hot die steel that is 4Cr5MoSiV1 to the trade mark in GB/T1299-2000 standard, when manufacture, first use plain-milling machine to process raw-material appearance and size, then use radial drill to get out hole for hoist, re-use the dovetail gradient that CNC milling machine mills out the back side, and rough mill die cavity and guide pad, 0.2 to 0.4 millimeter of monolateral allowance while rough milling, then at the temperature of 1050 to 1080 DEG C, heat-treat, use oil cooling or air cooling, tempering 2-3 time, temperature 53-560 DEG C, after processing, the Rockwell hardness of this mould reaches 48-52, the Rockwell hardness of cutting stamping head and trimming is 42-46, follow mould back side plain grinding until see light, then use CNC milling machine finish-milling die cavity and guide pad size, if any processing less than small round corner use electric spark electric machining, the finally wedge angle chamfered edge to mould.
The utility model is used for forging and pressing connection aerofoil profile saddle bracket, when use, first calculate the volume of required blank according to the size of saddle type bearing, and convert thereof into and forge with the specification of cylinder blank, then use bar cutting-off machine that whole cylinder blank is cut into the segment material that length is 82mm, above-mentioned segment material is put into intermediate-frequency heating furnace to be heated, be heated to 1180 DEG C～1280 DEG C, meanwhile, the utility model is arranged on forging press, and be preheated to 100 DEG C～300 DEG C, then at the die cavity of mould, on the surface of stitching surface and overflow launder, spray releasing agent, then the above-mentioned blank through heating is put into die cavity, start forging press and can forge and press out complete saddle bracket blank, solve the incomplete problem of blank in forging and stamping in the past, forge and press out after blank, carry out again trimming, the operations such as polishing and boring, can obtain saddle bracket finished product.
In a word, the utility model adds overflow to stop projection in counterdie, can limit whens forging and stamping blank from connecting wing both sides and the both sides of saddle bracket main body flow out, blank is flowed to the tip portion of connecting wing and the two end portions of saddle bracket main body, after guarantee forging and stamping, especially connecting wing is full complete for the each several part of saddle bracket, saves blocking operation, saves blank, enhance productivity, very practical.
Claims (6)
1. one kind connects aerofoil profile saddle bracket forge die, comprise upper die and lower die, described patrix has the upper impression (6) identical with the upper profile shape of saddle bracket, described counterdie has the lower impressions (2) identical with the lower profile shape of saddle bracket, the edge of described upper impression (6) and described lower impressions (2) is all surrounded with stitching surface (4), described upper die and lower die all have the overflow launder (5) for holding clout, it is characterized in that: described counterdie has four overflows and stops projection (1), described overflow stops that projection (1) is positioned at four angle positions that connecting wing (9) and saddle bracket main body are, described patrix has with described overflow and stops the groove (8) that projection (1) matches, described in when described patrix and described counterdie pressing, overflow stops between projection (1) and described groove (8) to have gap.
2. connection aerofoil profile saddle bracket forge die according to claim 1, is characterized in that described overflow stops that projection (1) is positioned between described overflow launder (5) and described stitching surface (4).
3. connection aerofoil profile saddle bracket forge die according to claim 1, while it is characterized in that described patrix and described counterdie pressing described in overflow stop between the side of projection (1) and end face and described groove (8) all there is the gap of 2 millimeters.
4. connection aerofoil profile saddle bracket forge die according to claim 1, is characterized in that four jiaos of described counterdie have guide pad (3), and four jiaos of described patrix have the guide pad groove (7) suitable with described guide pad (3).
5. connection aerofoil profile saddle bracket forge die according to claim 1, is characterized in that described overflow stops that projection (1) is four prism type, and its length is 15～40 millimeters, and width is 10～30 millimeters, is highly 6～20 millimeters.
6. connection aerofoil profile saddle bracket forge die according to claim 1, the material that it is characterized in that described patrix and described counterdie is H13 steel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420389339.0U CN203955990U (en) | 2014-07-15 | 2014-07-15 | Connect aerofoil profile saddle bracket forge die |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420389339.0U CN203955990U (en) | 2014-07-15 | 2014-07-15 | Connect aerofoil profile saddle bracket forge die |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203955990U true CN203955990U (en) | 2014-11-26 |
Family
ID=51916630
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420389339.0U Expired - Lifetime CN203955990U (en) | 2014-07-15 | 2014-07-15 | Connect aerofoil profile saddle bracket forge die |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203955990U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106862458A (en) * | 2017-01-19 | 2017-06-20 | 安徽铖友汽车零部件制造有限公司 | Forging mold based on fillet structure |
| CN106862457A (en) * | 2017-01-19 | 2017-06-20 | 安徽铖友汽车零部件制造有限公司 | Vapor-permeable type forging mold |
-
2014
- 2014-07-15 CN CN201420389339.0U patent/CN203955990U/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106862458A (en) * | 2017-01-19 | 2017-06-20 | 安徽铖友汽车零部件制造有限公司 | Forging mold based on fillet structure |
| CN106862457A (en) * | 2017-01-19 | 2017-06-20 | 安徽铖友汽车零部件制造有限公司 | Vapor-permeable type forging mold |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee | ||
| CP03 | Change of name, title or address |
Address after: The city of Xinji East Street 052360 city in Hebei province Shijiazhuang City No. 0159 Patentee after: HEBEI TENGYUE RAILWAY EQUIPMENT CO.,LTD. Address before: City Street East Xinji city 052360 Hebei city of Shijiazhuang Province Patentee before: HEBEI XINJI TENGYUE INDUSTRIAL CO.,LTD. |
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| TR01 | Transfer of patent right |
Effective date of registration: 20230525 Address after: 050000 No. 0159 Shifu East Street, Xinji City, Shijiazhuang City, Hebei Province Patentee after: HEBEI TENGYUE RAILWAY EQUIPMENT CO.,LTD. Patentee after: Hebei Tengyue Railway Vehicle Parts Technology Co.,Ltd. Address before: 052360 No. 0159 Shifu East Street, Xinji City, Shijiazhuang City, Hebei Province Patentee before: HEBEI TENGYUE RAILWAY EQUIPMENT CO.,LTD. |
|
| TR01 | Transfer of patent right |