CN108927417B - Hot extrusion forming die and forming method for special-shaped deep-cavity complex-structure support - Google Patents

Hot extrusion forming die and forming method for special-shaped deep-cavity complex-structure support Download PDF

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CN108927417B
CN108927417B CN201810507707.XA CN201810507707A CN108927417B CN 108927417 B CN108927417 B CN 108927417B CN 201810507707 A CN201810507707 A CN 201810507707A CN 108927417 B CN108927417 B CN 108927417B
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die
hot extrusion
guide
guide post
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CN108927417A (en
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王胜龙
郭晓琳
王志敏
吴凯
东栋
周小京
尤逢海
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Beijing Hangxing Machinery Manufacturing Co Ltd
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Beijing Hangxing Machinery Manufacturing Co Ltd
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21CMANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES, PROFILES OR LIKE SEMI-MANUFACTURED PRODUCTS OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
    • B21C25/00Profiling tools for metal extruding
    • B21C25/02Dies
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21CMANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES, PROFILES OR LIKE SEMI-MANUFACTURED PRODUCTS OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
    • B21C23/00Extruding metal; Impact extrusion
    • B21C23/001Extruding metal; Impact extrusion to improve the material properties, e.g. lateral extrusion
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21CMANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES, PROFILES OR LIKE SEMI-MANUFACTURED PRODUCTS OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
    • B21C25/00Profiling tools for metal extruding
    • B21C25/02Dies
    • B21C25/025Selection of materials therefor

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  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Forging (AREA)
  • Extrusion Of Metal (AREA)

Abstract

The hot extrusion forming die comprises an upper die, a lower die, a guide pillar and a guide sleeve, wherein the lower surface of the upper die and the upper surface of the lower die are horizontal planes, a male die is arranged on the lower surface of the upper die, a female die corresponding to the male die is arranged on the upper surface of the lower die, the female die is integrally of a concave structure, a flash groove is arranged around the female die, a guide groove is respectively arranged around the flash groove, and a gap is formed between the male die and the female die after the male die and the female die are matched to form the shape of a support forging; guide post holes are correspondingly arranged at two diagonal positions of the upper die and the lower die, a guide sleeve is arranged in each guide post hole, the guide sleeves and the guide post holes are fastened in a press fit mode, and the guide posts are respectively inserted into the guide sleeves corresponding to the upper die and the lower die to position the upper die and the lower die; according to the invention, through the design of the male die, the female die, the flash groove and the diversion groove, the flow of the blank is controlled so as to control the dimensional precision of the bracket forging, and redundant blanks can be discharged.

Description

异形深腔复杂结构支架热挤压成形模具及成形方法Special-shaped deep cavity complex structure stent hot extrusion forming die and forming method

技术领域technical field

本发明涉及机械加工设备技术领域,尤其是一种异形深腔复杂结构支架热挤压成形模具。The invention relates to the technical field of mechanical processing equipment, in particular to a hot extrusion forming die for a special-shaped deep cavity complex structure bracket.

背景技术Background technique

国防安全的大趋势要求武器装备更新换代的响应速度越来越快、技战术指标越来越高,武器装备逐渐显现出结构轻量化、复杂化、一体化的特点,构件质强比要求不断提高,结构轻量化和高强度需求矛盾越来越突出。为满足上述需求,航天武器构件大量采用了轻质合金异形复杂薄壁结构。其中,某型号航天武器用支架的横截面为长方形,呈深腔结构,底面为中空弧形面,四周侧壁为立筋条,其中一条侧壁上带两个“耳朵”,零件截面积较大,材料分布不均匀,也不是传统的轴对称零件。The general trend of national defense and security requires that the response speed of weapons and equipment replacement is getting faster and faster, and the technical and tactical indicators are getting higher and higher. , the contradiction between structural lightweight and high-strength requirements is becoming more and more prominent. In order to meet the above requirements, a large number of light alloy special-shaped complex thin-walled structures are used in aerospace weapon components. Among them, the cross section of a certain type of space weapon bracket is rectangular, with a deep cavity structure, the bottom surface is a hollow arc surface, the surrounding side walls are vertical ribs, one of the side walls has two "ears", and the cross-sectional area of the part is relatively small. Large, uneven material distribution, and not traditional axisymmetric parts.

目前该异形深腔复杂结构支架多采用铸件机加制造。该方法存在严重的弊端,比如材料利用率常低于30%,材料耗费严重;铸件机械加工及热处理过程中产生变形,报废风险大,制造成本高。而热挤压近净成形技术可以很好地解决以上问题,使材料利用率大幅提高,零件的变形易于控制,所需机械加工时间大幅缩短,同时热挤压过程可以降低材料变形抗力,提高材料塑性,材料性能也可以得到进一步改善,获得力学性能良好的热挤压产品,可确保产品性能满足指标要求。此外,热挤压成形模具可重复使用,且使用寿命长,大幅降低生产成本。At present, the special-shaped deep cavity complex structure bracket is mostly manufactured by casting machining. This method has serious drawbacks, for example, the material utilization rate is often lower than 30%, and the material consumption is serious; the castings are deformed during machining and heat treatment, the risk of scrapping is high, and the manufacturing cost is high. The hot extrusion near-net-shape technology can solve the above problems well, greatly improve the material utilization rate, easy to control the deformation of the parts, and greatly shorten the required machining time. At the same time, the hot extrusion process can reduce the deformation resistance of the material and improve the material Plasticity and material properties can also be further improved, and hot extrusion products with good mechanical properties can be obtained, which can ensure that the product properties meet the index requirements. In addition, the hot extrusion forming die is reusable and has a long service life, which greatly reduces production costs.

发明内容SUMMARY OF THE INVENTION

本发明解决的技术问题是:克服现有技术的不足,提供了一种结构简单、能有效提高异形深腔复杂结构支架热挤压成形精度且使用稳定性高的热挤压成形模具。The technical problem solved by the present invention is: to overcome the deficiencies of the prior art, to provide a hot extrusion forming die with a simple structure, which can effectively improve the hot extrusion forming precision of the special-shaped deep cavity complex structure bracket and has high stability in use.

本发明的技术解决方案是:异形深腔复杂结构支架锻件热挤压成形模具包括上模、下模、导柱和导套,上模的下表面及下模的上表面为水平面,在上模的下表面设置有凸模,在下模的上表面设置有与凸模对应的凹模,凹模整体为内凹结构,凹模周围设置有飞边槽,飞边槽四周各设置有一个导流槽,凸模与凹模配合后二者之间存在间隙,形成支架锻件的形状;分别在上模和下模对角线的两个角位置对应设置有导柱孔,在每个导柱孔内设置有导套,导套和导柱孔采用压配合紧固,通过分别将导柱插入在上模和下模对应的导套内,对上下模进行定位,导柱与导套之间留有0.15mm~0.5mm的间隙;在上模和下模内分别设置有9个加热管孔和3个热电偶孔。The technical solution of the present invention is: the hot extrusion forming die for the special-shaped deep cavity complex structure bracket forging includes an upper die, a lower die, a guide post and a guide sleeve, the lower surface of the upper die and the upper surface of the lower die are horizontal The lower surface of the die is provided with a punch, and the upper surface of the lower die is provided with a concave die corresponding to the punch. The concave die is a concave structure as a whole, and a flash groove is arranged around the concave die. Slot, there is a gap between the punch and the die after they are matched to form the shape of the bracket forging; guide post holes are correspondingly provided at the two corner positions of the upper die and the lower die diagonal, and each guide post hole is There is a guide sleeve inside, and the guide sleeve and the guide post hole are fastened by press fit. There is a gap of 0.15mm to 0.5mm; 9 heating tube holes and 3 thermocouple holes are respectively arranged in the upper die and the lower die.

优选凸模的凸起面、凹模的内凹面弧面半径均为467mm,凸模、凹模的整体拔模斜度为1°~10°,圆角半径为3mm~6mm。Preferably, the convex surface of the punch and the inner concave surface of the punch have a radius of 467mm, the overall draft angle of the punch and the punch is 1°-10°, and the fillet radius is 3mm-6mm.

优选所述的上模、下模所选用的材料为耐热钢、硬质合金或钢结硬质合金材料,导柱和导套所选用的材料为轴承钢、热作模具钢或者碳素工具钢材料。Preferably, the materials selected for the upper mold and the lower mold are heat-resistant steel, cemented carbide or steel-bonded cemented carbide materials, and the materials selected for the guide post and the guide sleeve are bearing steel, hot work die steel or carbon tools. steel material.

优选上模、下模、导柱和导套均需热处理,以提高强度、硬度及耐磨性能,延长模具使用寿命。Preferably, the upper mold, lower mold, guide post and guide sleeve need heat treatment to improve strength, hardness and wear resistance, and prolong the service life of the mold.

优选凸模、凹模、导柱孔、飞边槽、导流槽、导柱及导套的表面需打磨、抛光处理,以降低表面粗糙度,以利于脱模和提高锻件表面质量,凸模、凹模、飞边槽、导流槽的表面粗糙度Ra≤0.8,导柱Ra≤0.4,导套Ra≤0.8,导柱孔 Ra≤1.6。It is preferred that the surfaces of the punch, the die, the guide post hole, the flash groove, the guide groove, the guide post and the guide sleeve should be ground and polished to reduce the surface roughness, facilitate demolding and improve the surface quality of the forging. , The surface roughness of the die, flash groove and guide groove Ra≤0.8, guide post Ra≤0.4, guide sleeve Ra≤0.8, guide post hole Ra≤1.6.

本发明的异形深腔复杂结构支架锻件热挤压成形方法,其使用技术方案1-5 中任一项所述的异形深腔复杂结构支架锻件热挤压成形模具,该成型方法包括:步骤一,将轻质合金坯料放入下模的凹模内,步骤二,利用上模的凸模进行热挤压,挤压过程中坯料被挤压,同时将凸模与凹模配合后形成的型腔填充满,多余的坯料则从飞边槽内向外延伸,实现支架的热挤压精确成形,在热挤压成形过程中,通过导流槽可以将凸模与凹模配合后的封闭型腔内的空气排出,以提高支架锻件热挤压表面性能,步骤三,热挤压完成后,上模向上运动开模,取出锻件,支架热挤压工序完成。The hot extrusion forming method of the special-shaped deep cavity complex structure bracket forging of the present invention uses the hot extrusion forming die for the special-shaped deep cavity complex structure bracket forging described in any one of the technical solutions 1-5, and the forming method comprises: step 1 , put the light alloy billet into the concave die of the lower die, step 2, use the punch of the upper die to perform hot extrusion, the billet is extruded during the extrusion process, and at the same time the punch and the concave die are matched to form a mold The cavity is filled, and the excess billet extends outward from the flash groove to realize the precise hot extrusion forming of the bracket. The air in the cavity is exhausted to improve the hot extrusion surface performance of the bracket forging. In step 3, after the hot extrusion is completed, the upper die moves upward to open the mold, the forging is taken out, and the bracket hot extrusion process is completed.

本发明与现有技术相比的优点在于:The advantages of the present invention compared with the prior art are:

本发明通过凸模、凹模、飞边槽、导流槽的设计,能对坯料的流动进行控制从而保证支架锻件的尺寸精度,且能将多余的坯料排出,同时可提高模具的使用性能、稳定性和使用寿命,得到的锻件内部晶粒细小、组织致密,金属流线合理,表面质量良好,从而使得锻件的机械性能提高30%以上,同时无需对现有热挤压设备进行改造,结构简单,成本较低。The invention can control the flow of the blank through the design of the punch, the die, the flash groove and the guide groove, so as to ensure the dimensional accuracy of the bracket forging, and discharge the excess blank, and at the same time can improve the use performance of the mold, Stability and service life, the obtained forgings have small internal grains, dense structure, reasonable metal streamlines and good surface quality, so that the mechanical properties of the forgings can be improved by more than 30%, and there is no need to modify the existing hot extrusion equipment. Simple and low cost.

附图说明Description of drawings

图1为上模俯视图,Figure 1 is a top view of the upper die,

图2为上模立体图,Figure 2 is a perspective view of the upper die,

图3为下模俯视图,Figure 3 is a top view of the lower die,

图4为下模立体图,Figure 4 is a perspective view of the lower die,

图5为导柱示意图,Figure 5 is a schematic diagram of the guide post,

图6为导套示意图。Figure 6 is a schematic diagram of the guide sleeve.

具体实施方式Detailed ways

实施例1:Example 1:

如图1~6所示,本实施例所描述的的一种异形深腔复杂结构支架锻件热挤压成形模具,包括上模1、下模9、导柱13、导套14,上模1的下表面及下模9的上表面为水平面,在上模1的下表面设置有凸模2,在下模9的上表面设置有与凸模2对应的凹模10,凹模10整体为内凹结构,凹模10周围设置有飞边槽11,飞边槽11四周各设置有一个导流槽12,凸模2与凹模10配合后二者之间存在间隙,形成支架锻件的形状;采用双导柱,分别在上模1和下模9对角线的两个角位置设置有导柱孔3,导套14放在导柱孔3内,二者之间采用压配合紧固,导柱13放在导套14内,二者之间留有0.15mm的间隙;在上模1和下模9内分别设置有9个加热管孔7和3个热电偶孔6。凸模2的凸起面、凹模10的内凹面弧面半径均为467mm,凸模2、凹模10的整体拔模斜度为1°,圆角半径为5mm。上模1、下模9所选用的材料为低耐热高韧性钢5CrMnMo,导柱13和导套14所选用的材料为轴承钢SUJ12;上模1、下模9、导柱13和导套14经过热处理,具有足够的强度、硬度及耐磨性能;凸模2、凹模10、飞边槽11、导柱13及导套14的表面经过打磨、抛光处理,凸模、凹模、飞边槽、导流槽的表面粗糙度Ra0.8,导柱Ra0.4,导套Ra0.8,导柱孔Ra1.6。As shown in Figures 1 to 6, a hot extrusion forming die for a bracket forging with a special-shaped deep cavity complex structure described in this embodiment includes an upper die 1, a lower die 9, a guide post 13, a guide sleeve 14, an upper die 1 The lower surface of the lower die 9 and the upper surface of the lower die 9 are horizontal planes, a punch 2 is provided on the lower surface of the upper die 1, and a concave die 10 corresponding to the punch 2 is arranged on the upper surface of the lower die 9. In the concave structure, a flash groove 11 is provided around the concave die 10, and a diversion groove 12 is provided around the flash groove 11. After the punch 2 and the concave die 10 are matched, there is a gap between the two to form the shape of the bracket forging; Using double guide posts, guide post holes 3 are respectively provided at two diagonal corners of the upper die 1 and the lower die 9, the guide sleeve 14 is placed in the guide post holes 3, and the two are fastened by press fit. The guide post 13 is placed in the guide sleeve 14 with a gap of 0.15mm between them; 9 heating tube holes 7 and 3 thermocouple holes 6 are respectively arranged in the upper die 1 and the lower die 9 . The radii of the convex surface of the punch 2 and the inner concave surface of the die 10 are both 467mm, the overall draft angle of the punch 2 and the die 10 is 1°, and the radius of the fillet is 5mm. The material selected for the upper mold 1 and the lower mold 9 is low heat-resistant high-toughness steel 5CrMnMo, and the material selected for the guide post 13 and the guide sleeve 14 is bearing steel SUJ12; the upper mold 1, the lower mold 9, the guide post 13 and the guide sleeve 14 After heat treatment, it has sufficient strength, hardness and wear resistance; the surfaces of the punch 2, the die 10, the flash groove 11, the guide post 13 and the guide sleeve 14 have been ground and polished. The surface roughness of the side groove and the guide groove is Ra0.8, the guide post is Ra0.4, the guide sleeve is Ra0.8, and the guide post hole is Ra1.6.

在使用过程中,将5A06铝合金坯料放入下模9的凹模10内,利用上模1 的凸模2进行热挤压,挤压过程中坯料被挤压,同时将凹模10与凸模2配合后的型腔填充满,而多余的坯料则从飞边槽11内向外延伸,最终实现热挤压精确成形,而且能避免坯料对凸模2和凹模10边缘的挤压而造成的损坏,能有效提高模具的使用寿命,稳定性得到提升。在热挤压成形过程中,导流槽12 的设计可以将凸模2与凹模10配合后的封闭型腔内的空气排出,提高支架锻件热挤压表面性能。热挤压完成后,上模1向上运动开模,取出锻件,支架热挤压工序完成。将热挤压成形后的支架锻件转入后续工序,经热处理、机械加工等工序,最终加工为支架成品。During use, the 5A06 aluminum alloy billet is put into the concave die 10 of the lower die 9, and the punch 2 of the upper die 1 is used for hot extrusion. During the extrusion process, the billet is extruded, and the concave die 10 and the convex die The cavity after the mold 2 is matched is filled, and the excess blank extends from the flash groove 11 to the outside, and finally achieves accurate hot extrusion forming, and can avoid the extrusion of the blank on the edges of the punch 2 and the die 10. The damage can effectively improve the service life of the mold and improve the stability. In the process of hot extrusion, the design of the guide groove 12 can discharge the air in the closed cavity after the punch 2 and the die 10 are matched, so as to improve the hot extrusion surface performance of the bracket forging. After the hot extrusion is completed, the upper die 1 is moved upward to open the die, the forging is taken out, and the hot extrusion process of the bracket is completed. The bracket forgings formed by hot extrusion are transferred to the subsequent process, and are finally processed into bracket products after heat treatment, machining and other processes.

实施例2:Example 2:

如图1~6所示,本实施例所描述的的一种异形深腔复杂结构支架锻件热挤压成形模具,包括上模1、下模9、导柱13、导套14,上模1的下表面及下模9的上表面为水平面,在上模1的下表面设置有凸模2,在下模9的上表面设置有与凸模2对应的凹模10,凹模10整体为内凹结构,凹模10周围设置有飞边槽11,飞边槽11四周各设置有一个导流槽12,凸模2与凹模10配合后二者之间存在间隙,形成支架锻件的形状;采用双导柱,分别在上模1和下模9对角线的两个角位置设置有导柱孔3,导套14放在导柱孔3内,二者之间采用压配合紧固,导柱13放在导套14内,二者之间留有0.3mm的间隙;在上模1和下模9内分别设置有9个加热管孔7和3个热电偶孔6。凸模2的凸起面、凹模10的内凹面弧面半径均为467mm,凸模2、凹模10的整体拔模斜度为10°,圆角半径为6mm。上模1、下模9所选用的材料为中耐热韧性钢4Cr5MoSiV,导柱13和导套14所选用的材料为碳素工具钢T7;上模1、下模 9、导柱13和导套14经过热处理,具有足够的强度、硬度及耐磨性能;凸模2、凹模10、飞边槽11、导柱13及导套14的表面经过打磨、抛光处理,凸模、凹模、飞边槽、导流槽的表面粗糙度Ra0.4,导柱Ra0.4,导套Ra0.8,导柱孔Ra1.6。As shown in Figures 1 to 6, a hot extrusion forming die for a bracket forging with a special-shaped deep cavity complex structure described in this embodiment includes an upper die 1, a lower die 9, a guide post 13, a guide sleeve 14, an upper die 1 The lower surface of the lower die 9 and the upper surface of the lower die 9 are horizontal planes, a punch 2 is provided on the lower surface of the upper die 1, and a concave die 10 corresponding to the punch 2 is arranged on the upper surface of the lower die 9. In the concave structure, a flash groove 11 is provided around the concave die 10, and a diversion groove 12 is provided around the flash groove 11. After the punch 2 and the concave die 10 are matched, there is a gap between the two to form the shape of the bracket forging; Using double guide posts, guide post holes 3 are respectively provided at two diagonal corners of the upper die 1 and the lower die 9, the guide sleeve 14 is placed in the guide post holes 3, and the two are fastened by press fit. The guide post 13 is placed in the guide sleeve 14 with a gap of 0.3 mm between them; 9 heating tube holes 7 and 3 thermocouple holes 6 are respectively arranged in the upper die 1 and the lower die 9 . The radii of the convex surface of the punch 2 and the inner concave surface of the die 10 are both 467mm, the overall draft angle of the punch 2 and the die 10 is 10°, and the radius of the fillet is 6mm. The material selected for the upper mold 1 and the lower mold 9 is medium heat-resistant toughness steel 4Cr5MoSiV, and the material selected for the guide post 13 and the guide sleeve 14 is carbon tool steel T7; The sleeve 14 is heat-treated and has sufficient strength, hardness and wear resistance; the surfaces of the punch 2, the concave die 10, the flash groove 11, the guide post 13 and the guide sleeve 14 are ground and polished, and the punch, concave die, The surface roughness of the flash groove and the guide groove is Ra0.4, the guide post is Ra0.4, the guide sleeve is Ra0.8, and the guide post hole is Ra1.6.

在使用过程中,将VW63Z耐高温镁合金坯料放入下模9的凹模10内,利用上模1的凸模2进行热挤压,挤压过程中坯料被挤压,同时将凹模10与凸模2配合后的型腔填充满,而多余的坯料则从飞边槽11内向外延伸,最终实现热挤压精确成形,而且能避免坯料对凸模2和凹模10边缘的挤压而造成的损坏,能有效提高模具的使用寿命,稳定性得到提升。在热挤压成形过程中,导流槽12的设计可以将凸模2与凹模10配合后的封闭型腔内的空气排出,提高支架锻件热挤压表面性能。热挤压完成后,上模1向上运动开模,支架锻件卡在凹模10内部,利用撬棍通过导流槽12将锻件撬出,工件取下简单方便,效率高。将热挤压成形后的支架锻件转入后续工序,经热处理、机械加工等工序,最终加工为支架成品。During use, the VW63Z high temperature resistant magnesium alloy billet is put into the concave die 10 of the lower die 9, and the punch 2 of the upper die 1 is used for hot extrusion. During the extrusion process, the billet is extruded, while the concave die 10 is pressed. The cavity after being matched with the punch 2 is filled, and the excess blanks extend outward from the flash groove 11, so as to achieve accurate hot extrusion forming, and avoid the extrusion of the blanks on the edges of the punch 2 and the die 10. The damage caused can effectively improve the service life of the mold and improve the stability. In the process of hot extrusion, the design of the guide groove 12 can discharge the air in the closed cavity after the punch 2 and the die 10 are matched, so as to improve the hot extrusion surface performance of the bracket forging. After the hot extrusion is completed, the upper die 1 moves upward to open the die, the bracket forging is stuck inside the die 10, and the forging is pryed out through the guide groove 12 with a crowbar. The bracket forgings formed by hot extrusion are transferred to the subsequent process, and are finally processed into bracket products after heat treatment, machining and other processes.

经本发明人多次研究验证,上述导柱与导套之间的间隙可以在0.15mm~ 0.5mm之间进行选择,整体拔模斜度选择1°~10°圆角半径选择3mm~6mm,比较利于脱模。It has been verified by the inventor for many times that the gap between the above-mentioned guide post and the guide sleeve can be selected between 0.15mm and 0.5mm, and the overall draft angle can be selected from 1° to 10° and the radius of the fillet can be selected from 3mm to 6mm. It is more conducive to demoulding.

如上所述即为本发明的实施例。本发明不局限于上述实施方式,任何人应该得知在本发明的启示下做出的结构变化,凡是与本发明具有相同或相近的技术方案,均落入本发明的保护范围之内。The above are the embodiments of the present invention. The present invention is not limited to the above-mentioned embodiments, and anyone should know that structural changes made under the inspiration of the present invention, and all technical solutions that are the same or similar to those of the present invention, fall within the protection scope of the present invention.

本发明说明书中未作详细描述的内容属本领域技术人员的公知技术。The content not described in detail in the specification of the present invention belongs to the well-known technology of those skilled in the art.

Claims (10)

1.异形深腔复杂结构支架锻件热挤压成形模具,其特征在于:包括上模、下模、导柱和导套,上模的下表面及下模的上表面为水平面,在上模的下表面设置有凸模,在下模的上表面设置有与凸模对应的凹模,凹模整体为内凹结构,凹模周围设置有飞边槽,飞边槽四周各设置有一个导流槽,凸模与凹模配合后二者之间存在间隙,形成支架锻件的形状;分别在上模和下模对角线的两个角位置对应设置有导柱孔,在每个导柱孔内设置有导套,导套和导柱孔采用压配合紧固,通过分别将导柱插入在上模和下模对应的导套内,对上下模进行定位;导柱与导套之间留有间隙;在上模和下模内分别设置有加热管孔和热电偶孔。1. special-shaped deep cavity complex structure bracket forging hot extrusion forming die, it is characterized in that: comprise upper die, lower die, guide post and guide sleeve, the lower surface of the upper die and the upper surface of the lower die are horizontal planes, in the upper die The lower surface is provided with a punch, and the upper surface of the lower die is provided with a concave die corresponding to the punch. The concave die is a concave structure as a whole, a flash groove is arranged around the concave die, and a diversion groove is arranged around the flash groove. , after the punch and the die are matched, there is a gap between the two to form the shape of the bracket forging; guide post holes are correspondingly arranged at the two corner positions of the upper die and the lower die diagonal, and in each guide post hole A guide sleeve is provided, and the guide sleeve and the guide post hole are fastened by press fit. By inserting the guide post into the corresponding guide sleeve of the upper die and the lower die, the upper and lower dies are positioned; there is a space between the guide post and the guide sleeve. Gap; heating tube holes and thermocouple holes are respectively arranged in the upper die and the lower die. 2.根据权利要求1所述的异形深腔复杂结构支架锻件热挤压成形模具,其特征在于:所述导柱与导套之间留有的间隙为0.15mm~0.5mm。2 . The hot extrusion forming die for a special-shaped deep cavity complex structure bracket forging according to claim 1 , wherein the gap between the guide post and the guide sleeve is 0.15 mm to 0.5 mm. 3 . 3.根据权利要求1所述的异形深腔复杂结构支架锻件热挤压成形模具,其特征在于:所述加热管孔设置有九个。3 . The hot extrusion forming die for a special-shaped deep cavity complex structure bracket forging according to claim 1 , wherein the heating tube holes are provided with nine holes. 4 . 4.根据权利要求1所述的异形深腔复杂结构支架锻件热挤压成形模具,其特征在于:所述热电偶孔设置有三个。4 . The hot extrusion forming die for a special-shaped deep cavity complex structure bracket forging according to claim 1 , wherein three thermocouple holes are provided. 5 . 5.根据权利要求1所述的异形深腔复杂结构支架锻件热挤压成形模具,其特征在于:凸模的凸起面、凹模的内凹面弧面半径均为467mm,凸模、凹模的整体拔模斜度为1°~10°,圆角半径为3mm~6mm。5. The special-shaped deep cavity complex structure bracket forging hot extrusion forming die according to claim 1 is characterized in that: the convex surface of the punch and the inner concave surface radius of the concave die are 467mm, and the punch and the concave die are both 467mm. The overall draft angle is 1° to 10°, and the fillet radius is 3mm to 6mm. 6.根据权利要求1所述的异形深腔复杂结构支架锻件热挤压成形模具,其特征在于:所述的上模、下模所选用的材料为耐热钢、硬质合金或钢结硬质合金材料,导柱和导套所选用的材料为轴承钢、热作模具钢或者碳素工具钢材料。6. The special-shaped deep cavity complex structure bracket forging hot extrusion forming die according to claim 1, characterized in that: the materials selected for the upper die and the lower die are heat-resistant steel, cemented carbide or hardened steel The material used for the guide post and guide bush is bearing steel, hot work die steel or carbon tool steel. 7.根据权利要求1所述的异形深腔复杂结构支架锻件热挤压成形模具,其特征在于:对上模、下模、导柱和导套进行热处理。7 . The hot extrusion forming die for special-shaped deep cavity complex structure bracket forgings according to claim 1 , wherein the upper die, the lower die, the guide post and the guide sleeve are heat-treated. 8 . 8.根据权利要求1所述的异形深腔复杂结构支架锻件热挤压成形模具,其特征在于:对凸模、凹模、导柱孔、飞边槽、导流槽、导柱及导套的表面进行打磨、抛光处理。8. The special-shaped deep cavity complex structure bracket forging hot extrusion forming die according to claim 1, characterized in that: the punch, the die, the guide post hole, the flash groove, the guide groove, the guide post and the guide sleeve The surface is ground and polished. 9.根据权利要求8所述的异形深腔复杂结构支架锻件热挤压成形模具,其特征在于:所述凸模、凹模、飞边槽、导流槽的表面粗糙度Ra≤0.8,导柱Ra≤0.4,导套Ra≤0.8,导柱孔Ra≤1.6。9. The hot extrusion forming die for special-shaped deep cavity complex structure bracket forgings according to claim 8, characterized in that: the surface roughness of the punch, the die, the flash groove and the guide groove is Ra≤0.8, and the guide Post Ra≤0.4, guide sleeve Ra≤0.8, guide post hole Ra≤1.6. 10.异形深腔复杂结构支架锻件热挤压成形方法,其使用权利要求1~9中任一项所述的异形深腔复杂结构支架锻件热挤压成形模具,其特征在于:包括如下步骤:10. A method for hot extrusion forming of special-shaped deep cavity complex structure bracket forgings, which uses the special-shaped deep cavity complex structure bracket forgings hot extrusion forming die according to any one of claims 1 to 9, characterized in that: comprising the following steps: 步骤一,将轻质合金坯料放入下模的凹模内;Step 1, put the light alloy blank into the concave die of the lower die; 步骤二,利用上模的凸模进行热挤压,挤压过程中坯料被挤压,同时将凸模与凹模配合后形成的型腔填充满,多余的坯料则从飞边槽内向外延伸,实现支架的热挤压精确成形;The second step is to use the punch of the upper die for hot extrusion. During the extrusion process, the blank is extruded, and at the same time, the cavity formed by the combination of the punch and the concave die is filled, and the excess blank is sent from the flash groove to the outside. Extension, to achieve precise hot extrusion forming of the stent; 步骤三,热挤压完成后,上模向上运动开模,取出锻件,支架热挤压工序完成。Step 3: After the hot extrusion is completed, the upper die is moved upward to open the die, the forging is taken out, and the hot extrusion process of the bracket is completed.
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