CN115488181A - Uniform extrusion forming die for magnesium-aluminum alloy section - Google Patents
Uniform extrusion forming die for magnesium-aluminum alloy section Download PDFInfo
- Publication number
- CN115488181A CN115488181A CN202211221359.2A CN202211221359A CN115488181A CN 115488181 A CN115488181 A CN 115488181A CN 202211221359 A CN202211221359 A CN 202211221359A CN 115488181 A CN115488181 A CN 115488181A
- Authority
- CN
- China
- Prior art keywords
- cavity
- groove
- flow
- groove surface
- main cavity
- 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
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE 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
- B21C25/00—Profiling tools for metal extruding
- B21C25/02—Dies
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21C—MANUFACTURE 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
- B21C23/00—Extruding metal; Impact extrusion
- B21C23/02—Making uncoated products
- B21C23/04—Making uncoated products by direct extrusion
- B21C23/14—Making other products
- B21C23/142—Making profiles
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Extrusion Of Metal (AREA)
Abstract
本发明公开一种镁铝合金型材均匀挤压成形模具,包括安装在压力机上模板下方的凸模组件、安装在压力机下模板上方的凹模组件;凸模组件形成有向下凸起的凸模主体;凹模组件在正对凸模主体下方形成有顶部开口的容料腔,容料腔供坯料置入并供凸模主体向下插入,容料腔的腔底形成挤压面,挤压面向下导通形成有主型腔和连通在主型腔四周的多个翼片型腔,主型腔和多个翼片型腔共同形成与工件对应的轮廓,挤压面在每相邻两个翼片型腔之间分别下凹形成有一个限流凹槽,每个限流凹槽在靠近主型腔侧形成限制坯料流向主型腔的第一槽面、在靠近翼片型腔侧形成限制坯料流向翼片型腔的第二槽面。本发明使坯料在挤压成形过程中能够均匀流向主型腔和翼片型腔。
The invention discloses a mold for uniform extrusion of magnesium-aluminum alloy profiles, which comprises a punch assembly installed below the upper template of the press, and a die assembly installed above the lower template of the press; the punch assembly is formed with a downward convex The main body of the punch is raised; the die assembly forms a material-holding cavity with a top opening directly below the main body of the punch. Pressing surface, the extrusion surface is connected downwards to form a main cavity and multiple fin cavities connected around the main cavity. The main cavity and multiple fin cavities together form a contour corresponding to the workpiece. The extrusion surface A flow-limiting groove is recessed between every two adjacent fin cavities, and each flow-limiting groove forms a first groove surface on the side close to the main cavity to limit the flow of the blank to the main cavity, and on the side close to the main cavity. The side of the airfoil cavity forms a second groove surface that restricts the flow of the blank to the airfoil cavity. The invention enables the blank to flow uniformly to the main die cavity and the airfoil die cavity during the extrusion forming process.
Description
技术领域technical field
本发明涉及挤压成形模具技术领域,特别涉及一种镁铝合金型材均匀挤压成形模具。The invention relates to the technical field of extrusion molding dies, in particular to a uniform extrusion molding die for magnesium-aluminum alloy profiles.
背景技术Background technique
正挤压成形技术是一种常用的镁合金塑性成形技术,经过挤压变形获得的镁合金产品具有材料利用率高、成形精度高、生产效率高等一系列优点。Forward extrusion forming technology is a commonly used plastic forming technology for magnesium alloys. Magnesium alloy products obtained through extrusion deformation have a series of advantages such as high material utilization rate, high forming precision, and high production efficiency.
但是正挤压成形通常存在以下问题:坯料在充入模具型腔的过程中,由于型腔内各处对坯料的流动限制不均,造成坯料充满型腔后金属流线不均匀,导致最终制得的工件残余应力较大,并且微观组织和力学性能各向异性较大,在工件使用过程中容易沿力学性能差的部位失效,降低了工件的使用寿命;However, there are usually the following problems in forward extrusion molding: when the billet is filled into the mold cavity, due to the uneven flow restrictions on the billet in the cavity, the metal flow line after the billet is filled with the cavity is uneven, resulting in the final production. The residual stress of the obtained workpiece is relatively large, and the anisotropy of the microstructure and mechanical properties is relatively large, and it is easy to fail along the parts with poor mechanical properties during the use of the workpiece, which reduces the service life of the workpiece;
尤其是针对形状复杂的工件,例如在工件主体外周设置有薄翼片的工件,由于型腔在翼片处体积较小、宽度较窄,而在工件主体处体积较大、宽度较大,导致坯料不易流向型腔的翼片处,最终制得工件的力学性能将大受影响。Especially for workpieces with complex shapes, such as workpieces with thin fins on the outer periphery of the workpiece body, the cavity is small in volume and narrow in width at the fins, and large in volume and wide in the body of the workpiece, resulting in The billet is not easy to flow to the fins of the cavity, and the mechanical properties of the final workpiece will be greatly affected.
发明内容Contents of the invention
本发明的目的在于提供一种镁铝合金型材均匀挤压成形模具,克服上述缺陷,使坯料在挤压成形过程中能够均匀地流向型腔的翼片处和工件主体处。The purpose of the present invention is to provide a magnesium-aluminum alloy profile uniform extrusion molding die, which overcomes the above-mentioned defects, so that the billet can evenly flow to the fins of the cavity and the main body of the workpiece during the extrusion molding process.
为达成上述目的,本发明的解决方案为:一种镁铝合金型材均匀挤压成形模具,包括安装在压力机上模板下方的凸模组件、安装在压力机下模板上方的凹模组件;In order to achieve the above object, the solution of the present invention is: a magnesium-aluminum alloy profile uniform extrusion forming die, including a punch assembly installed below the upper template of the press, and a die assembly installed above the lower template of the press;
所述凸模组件形成有向下凸起的凸模主体;The punch assembly is formed with a downwardly protruding punch body;
所述凹模组件在正对所述凸模主体下方形成有顶部开口的容料腔,所述容料腔供坯料置入并供所述凸模主体向下插入,所述容料腔的腔底形成挤压面,所述挤压面向下导通形成有主型腔和连通在所述主型腔四周的多个翼片型腔,所述主型腔和多个所述翼片型腔共同形成与工件对应的轮廓,所述挤压面在每相邻两个翼片型腔之间分别下凹形成有一个限流凹槽,每个所述限流凹槽在靠近所述主型腔侧形成限制坯料流向主型腔的第一槽面、在靠近所述翼片型腔侧形成限制坯料流向翼片型腔的第二槽面。The die assembly is formed directly below the main body of the male mold with a top-opened material chamber for the blank to be placed and for the male mold body to be inserted downwards. The bottom of the cavity forms an extrusion surface, and the extrusion surface leads downward to form a main cavity and a plurality of fin cavities connected around the main cavity. The main cavity and a plurality of fins The cavities together form a contour corresponding to the workpiece, and the extrusion surface is recessed between every two adjacent fin cavities to form a flow-limiting groove, and each of the flow-limiting grooves is close to the main A first groove surface is formed on the side of the cavity to limit the flow of the blank to the main cavity, and a second groove surface is formed on the side close to the cavity of the fin to limit the flow of the blank to the cavity of the fin.
进一步,所述主型腔为纵向延伸的圆柱形腔体,所述翼片型腔为纵向延伸的长方体形腔体,所述限流凹槽的横截面呈扇形,一个限流凹槽的两个第二槽面间水平方向的夹角大于或小于与该限流凹槽相邻的两个翼片型腔间水平方向的夹角。Further, the main cavity is a longitudinally extending cylindrical cavity, the fin cavity is a longitudinally extending cuboid cavity, the cross section of the flow limiting groove is fan-shaped, and the two flow limiting grooves The included angle in the horizontal direction between the two second groove surfaces is larger or smaller than the included angle in the horizontal direction between the two fin cavities adjacent to the flow limiting groove.
进一步,所述第一槽面顶部朝向所述主型腔倾斜,所述第二槽面顶部朝向与其相邻的翼片型腔倾斜,所述第一槽面的倾斜角度大于或小于所述第二槽面的倾斜角度。Further, the top of the first groove surface is inclined toward the main cavity, the top of the second groove surface is inclined toward the fin cavity adjacent thereto, and the inclination angle of the first groove surface is larger or smaller than that of the second groove surface. The inclination angle of the second groove surface.
进一步,所述挤压面呈中间低四周高或中间高四周低的锥形面,所述主型腔顶端导通在所述挤压面中央。Further, the extrusion surface is a tapered surface with a low middle and high surroundings or a high middle and low surroundings, and the top of the main cavity is connected to the center of the extrusion surface.
进一步,所述限流凹槽背离所述主型腔侧形成第三槽面,所述第三槽面的高度大于或小于所述第一槽面的高度。Further, a third groove surface is formed on the side of the flow limiting groove facing away from the main cavity, and the height of the third groove surface is greater than or smaller than that of the first groove surface.
进一步,所述限流凹槽背离所述主型腔侧形成第三槽面,所述第一槽面顶部朝向主型腔侧倾斜,所述第三槽面顶部朝向背离主型腔侧倾斜,所述第一槽面的倾斜角度大于或小于所述第三槽面的倾斜角度。Further, the flow limiting groove forms a third groove surface away from the side of the main cavity, the top of the first groove surface is inclined toward the side of the main cavity, and the top of the third groove surface is inclined toward the side away from the main cavity, The inclination angle of the first groove surface is larger or smaller than the inclination angle of the third groove surface.
进一步,所述第一槽面的长度大于或小于所述第二槽面的长度。Further, the length of the first groove surface is greater than or smaller than the length of the second groove surface.
进一步,所述第一槽面、第二槽面、第三槽面、挤压面间平滑过渡。Further, the transition between the first groove surface, the second groove surface, the third groove surface and the extrusion surface is smooth.
进一步,所述凸模主体底部下凸形成有一根型芯杆,所述型芯杆用于向下插入所述主型腔,并与所述主型腔侧壁之间留有供坯料流入的间隙。Further, the bottom of the main body of the punch is convexly formed with a core rod, the core rod is used to insert downward into the main cavity, and there is a gap between the main cavity side wall and the main cavity for the blank to flow in. gap.
进一步,所述压力机下模板上纵向滑动安装有顶杆,所述顶杆位于所述主型腔底部,以在向上插入主型腔时上顶出工件。Further, a ejector pin is longitudinally slidably installed on the lower mold plate of the press, and the ejector pin is located at the bottom of the main cavity, so as to push out the workpiece when it is inserted upward into the main cavity.
采用上述方案后,本发明的有益效果在于:凹模组件在正对凸模主体下方形成有顶部开口的容料腔,容料腔供坯料置入并供凸模主体向下插入,容料腔的腔底形成挤压面,挤压面向下导通形成有主型腔和连通在主型腔四周的多个翼片型腔,主型腔和多个翼片型腔共同形成与工件对应的轮廓,当凸模主体插入容料腔时,推挤容料腔内的坯料变形后流入主型腔和各翼片型腔,挤压面在每相邻两个翼片型腔之间分别下凹形成有一个限流凹槽,每个限流凹槽在靠近主型腔侧形成限制坯料流向主型腔的第一槽面、在靠近翼片型腔侧形成限制坯料流向限流凹槽的第二槽面,通过将第一槽面和第二槽面配置成不同的倾角、高度、长度等,使坯料流在向主型腔和各翼片型腔时具有不同程度的流动限制,进而平衡坯料流向主型腔和各翼片型腔的流速,实现均匀挤压成形。After adopting the above scheme, the beneficial effect of the present invention is that: the die assembly forms a material-holding chamber with a top opening directly below the main body of the punch. The bottom of the cavity forms an extrusion surface, and the extrusion surface is connected downward to form a main cavity and multiple fin cavities connected around the main cavity. The main cavity and multiple fin cavities jointly form a When the main body of the punch is inserted into the material cavity, the billet in the material cavity is deformed and flows into the main cavity and each fin cavity, and the extrusion surface is separated between each adjacent two fin cavities. A flow-limiting groove is formed in the depression, and each flow-limiting groove forms a first groove surface that restricts the flow of the blank to the main cavity on the side close to the main cavity, and a flow-limiting groove that restricts the flow of the blank to the main cavity on the side close to the fin cavity. The second groove surface, by configuring the first groove surface and the second groove surface to have different inclination angles, heights, lengths, etc., the blank flow has different degrees of flow restriction when it flows to the main cavity and each fin cavity, Then the flow velocity of the billet flowing to the main cavity and each wing cavity is balanced to realize uniform extrusion.
附图说明Description of drawings
图1为本发明中工件成形后的俯视结构示意图;Fig. 1 is the top view structure schematic diagram after workpiece forming among the present invention;
图2为本发明中凹模模芯的俯视结构示意图;Fig. 2 is the top view structural representation of die core in the present invention;
图3为本发明中凹模模芯的俯视断面结构示意图;Fig. 3 is the top view sectional structure schematic diagram of die core in the present invention;
图4为本发明h3大于h1时限流凹槽沿凹模模芯径向的截面结构示意图;Fig. 4 is a schematic cross-sectional structure diagram of the flow-limiting groove along the radial direction of the die core when h3 of the present invention is greater than h1;
图5为本发明入料前的模具结构示意图;Fig. 5 is the mold structure schematic diagram before charging of the present invention;
图6为本发明入料后的模具结构示意图;Fig. 6 is the mold structure schematic diagram after charging of the present invention;
图7为本发明穿孔后模具结构示意图;Fig. 7 is a schematic diagram of the structure of the mold after perforation according to the present invention;
图8为本发明成形后的模具结构示意图;Fig. 8 is the schematic diagram of the mold structure after forming of the present invention;
图9为本发明省略压力机上模板和凸模组件后顶杆顶出工件和凹模模芯的模具结构示意图;Fig. 9 is a schematic diagram of the mold structure in which the ejector rod ejects the workpiece and the die core after omitting the upper template and punch assembly of the press in the present invention;
图10为本发明凹模模芯装入凹模套筒的立体结构示意图。Fig. 10 is a three-dimensional structural schematic view of the die core of the present invention being loaded into the die sleeve.
标号说明:1-压力机上模板,2-凸模组件,3-压力机下模板,4-凹模组件,5-凸模主体,6-容料腔,7-坯料,8-挤压面,9-主型腔,10-翼片型腔,11-工件,12-限流凹槽,13-第一槽面,14-第二槽面,15-第三槽面,16-型芯杆,17-顶杆,18-轴孔,19-凹模模芯,20-凹模套筒。Explanation of symbols: 1-upper die plate of press machine, 2-punch die assembly, 3-lower die plate of press machine, 4-die die assembly, 5-punch die main body, 6-material chamber, 7-billet, 8-extrusion Surface, 9-main cavity, 10-wing cavity, 11-workpiece, 12-limiting groove, 13-first groove surface, 14-second groove surface, 15-third groove surface, 16-type Core rod, 17-ejector pin, 18-axis hole, 19-die mold core, 20-die sleeve.
具体实施方式detailed description
以下结合附图及具体实施例对本发明做详细的说明。The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.
本发明提供一种镁铝合金型材均匀挤压成形模具,如图1-10所示,包括安装固定在压力机上模板1下方的凸模组件2、安装固定在压力机下模板3上方的凹模组件4,压力机驱动压力机上模板1与压力机下模板3开合运动,进而带动所述凸模组件2与凹模组件4开合运动;The present invention provides a magnesium-aluminum alloy profile uniform extrusion molding die, as shown in Fig. Die assembly 4, the press drives the upper platen 1 of the press and the
所述凸模组件2形成有向下凸起的凸模主体5,所述凸模主体5呈圆柱体;所述凹模组件4在正对所述凸模主体5下方形成有顶部开口的容料腔6,所述容料腔6呈直径略大于所述凸模主体5的圆柱形腔,所述容料腔6供坯料7置入并供所述凸模主体5向下插入,所述容料腔6的腔底形成挤压面8,所述挤压面8向下导通形成有主型腔9和连通在所述主型腔9四周的多个翼片型腔10,所述主型腔9为纵向延伸的圆柱形腔体,各所述翼片型腔10均为纵向延伸的长方体形腔体,进而所述主型腔9和多个所述翼片型腔10共同形成与工件11对应的轮廓,本实施例中,所述工件11顶部中央还向下导通形成有一个轴孔18,为同时一次成型出所述轴孔18,所述凸模主体5底部下凸形成有一根型芯杆16,所述型芯杆16随凸模主体5下行,在位于容料腔6内的坯料7上冲出所述轴孔18,而后在凸模主体5继续下行时,所述型芯杆16用于向下插入所述主型腔9,并与所述主型腔9侧壁之间留有供坯料7流入的间隙,更具体地实施例中,为便于凹模组件4的制造,所述凹模组件4包括凹模模芯19和凹模套筒20,凹模套筒20呈圆筒形,凹模模芯19顶面形成所述挤压面8,所述主型腔9和翼片型腔10均开设在所述凹模模芯19上,所述凹模模芯19同轴且周向固定在所述凹模套筒20内,如图2、图3、图10所示,所述挤压面8可以呈平面,优选地实施例中,为使坯料7更易流入主型腔9和翼片型腔10,如图5-9所示,所述挤压面8的边缘还可以设置成向内倾斜的斜面,不具体限定;The
受所述主型腔9和翼片型腔10形状和位置的限制,坯料7在受挤压后,流入主型腔9和翼片型腔10的阻力不同,导致坯料7流向主型腔9和翼片型腔10的速度不同,为平衡坯料7向主型腔9和翼片型腔10流动的速度,所述挤压面8在每相邻两个翼片型腔10之间分别下凹形成有一个限流凹槽12,为配合所述主型腔9和翼片型腔10在挤压面8上形成的轮廓,所述限流凹槽12的横截面呈扇形,每个所述限流凹槽12在靠近所述主型腔9侧形成限制坯料7流向主型腔9的第一槽面13、在靠近所述翼片型腔10侧形成限制坯料7流向翼片型腔10的第二槽面14、在背离所述主型腔9侧形成限制坯料7向背离主型腔9的方向流动的第三槽面15,所述第一槽面13、第二槽面14、第三槽面15、挤压面8间平滑过渡,通过调整所述第一槽面13、第二槽面14和第三槽面15的位置以及形状,进而调整坯料7朝向各个方向流动时的阻力,使坯料均匀流入主型腔9和翼片型腔10,成型后的工件11金属流线将更加均匀,改善了工件11的力学性能各向异性的问题,实现提升材料的综合力学性能。Restricted by the shape and position of the
具体在本实施例中,此处重点结合图2-4所示,所述第一槽面13的高度为h1、长度L1,所述第一槽面13顶部朝向主型腔9倾斜θ1角度,并与所述主型腔9之间间隔d1距离;各所述第二槽面14的长度均为L2,且顶部朝向与其相邻的翼片型腔10倾斜θ2角度(θ2附图中未给出),并同与其相邻的翼片型腔10之间间隔d2距离,且同一限流凹槽12上的两个第二槽面14间水平方向的夹角为w;所述第三槽面15的高度为h3,所述第三槽面15朝向背离所述主型腔9侧倾斜θ3角度。Specifically, in this embodiment, as shown in Figures 2-4, the height of the
一个限流凹槽12的两个第二槽面14间水平方向的夹角w大于或小于与该限流凹槽12相邻的两个翼片型腔10间水平方向的夹角,重点参阅图3所示,具体地,当一个限流凹槽12的两个第二槽面14间水平方向的夹角w大于与该限流凹槽12相邻的两个翼片型腔10间水平方向的夹角时,第二槽面14远离主型腔9的一端相较靠近主型腔9的一端距离翼片型腔10更近,使得坯料7在继续受挤压时,处于限流凹槽12内的部分沿第二槽面14爬升出限流凹槽12后,继续横向流向与其相邻的翼片型腔10时,更快流入该翼片型腔10远离主型腔9的一端;反之,当一个限流凹槽12的两个第二槽面14间水平方向的夹角w小于与该限流凹槽12相邻的两个翼片型腔10间水平方向的夹角时,则更快流入翼片型腔10靠近主型腔9的一端,夹角w的实际角度根据实际成形效果具体调整。The angle w in the horizontal direction between the two
所述第一槽面13的倾斜角度θ1大于或小于所述第二槽面14的倾斜角度θ2,具体地,由于第一槽面13和第二槽面14的倾斜角度越小,对坯料7沿对应方向横向流动产生的阻力越大,当θ1大于θ2时,使得坯料7更易向第一槽面13所在方向流动,进而更快流向第一槽面13旁侧的主型腔9;反之,当θ1小于θ2时,使得坯料7更易向第二槽面14所在方向流动,进而更快流向第二槽面14旁侧的翼片型腔10,θ1和θ2的具体数值更具实际成形效果具体设定。The inclination angle θ1 of the
重点结合图4所示,所述第三槽面15的高度h3大于或小于所述第一槽面13的高度h1,具体地,由于第三槽面15和第一槽面13的高度越大,对坯料7沿对应方向横向流动产生的阻力越大,当h3大于h1时,使得坯料7更易向主型腔9流动,反之,当h3小于h1时,使得坯料7更易向背离主型腔9方向流动,进而更易流向主型腔9四周的翼片型腔10,h3和h1的具体数值更具实际成形效果具体设定。As shown in Fig. 4, the height h3 of the
重点结合图4所示,所述第一槽面13的倾斜角度θ1大于或小于所述第三槽面15的倾斜角度θ3,具体地,由于第三槽面15和第一槽面13的倾斜角度越大,对坯料7沿对应方向横向流动产生的阻力越小,当θ1大于θ3时,使得坯料7更易向主型腔9流动,反之,当θ1小于θ3时,使得坯料7更易向背离主型腔9方向流动,进而更易流向主型腔9四周的翼片型腔10,θ1和θ3的具体数值更具实际成形效果具体设定。4, the inclination angle θ1 of the
所述第一槽面13的长度L1大于或小于所述第二槽面14的长度L2,具体地,由于第一槽面13和第二槽面14的长度越大,对坯料7沿对应方向横向流动产生的阻力越大,当L1大于L2时,使得坯料7更易向第一槽面13所在方向流动,进而更快流向第一槽面13旁侧的主型腔9;反之,当L1小于L2时,使得坯料7更易向第二槽面14所在方向流动,进而更快流向第二槽面14旁侧的翼片型腔10,L1和L2的具体数值更具实际成形效果具体设定。The length L1 of the
所述主型腔9顶端导通在所述挤压面8中央,所述挤压面8还可以呈中间低四周高或中间高四周低的锥形面(附图中未给出);在挤压面8呈中间低四周高时,坯料7更易向挤压面8中央流动,更快进入主型腔9;在挤压面8呈中间高四周低时,坯料7更易向挤压面8边缘流动,更快进入各翼片型腔10。The top of the
优选地实施例中,为方便坯料7在成形出工件11后的脱模,所述压力机下模板3上纵向滑动安装有顶杆17,所述顶杆17位于所述主型腔9底部,以在向上插入主型腔9时上顶出工件11。In a preferred embodiment, in order to facilitate the demoulding of the blank 7 after the
一种复杂型材正挤压均匀成形方法,包括以下步骤:A method for forward extrusion uniform forming of complex profiles, comprising the following steps:
S1、重点结合图5所示,架设上述镁铝合金型材均匀挤压成形模具;S1, combined with the focus shown in Figure 5, erect the above-mentioned magnesium-aluminum alloy profile uniform extrusion molding die;
S2、重点结合图6所示,入料:将坯料7放入容料腔6;S2. Focusing on the combination shown in Figure 6, feeding: put the blank 7 into the
S3、重点结合图7、图8所示,成形:使所述凸模主体5带动所述型芯杆16下行,使所述型芯杆16在位于容料腔6内的坯料7上冲出所述轴孔18,而后使凸模主体5继续下行压入所述容料腔6,以推挤容料腔6内的坯料7流入主型腔9和翼片型腔10,最终充满主型腔9和翼片型腔10形成工件11;S3. Focusing on Figure 7 and Figure 8, forming: make the punch
S4、重点结合图9所示,下料:使所述顶杆17上行,向上顶出所述工件11,将工件11取出,优选在本实施例中,为便于工件11的脱模,所述凹模模芯19可以设置成多瓣拼合而成的,拼合位置以及具体瓣数不具体限定,常规设置,本实施中不再具体阐述,从而在上顶出工件11时,使凹模模芯19与工件11一同上顶出所述凹模套筒20,再使凹模模芯19沿拼合处打开,从而能够更加方便地取出所述工件11;S4. Emphasis is combined with that shown in Figure 9, blanking: make the
S5、流速调整:在步骤S3过程中,若坯料7充满主型腔9的速度大于充满翼片型腔10的速度,则增大L1/L2的比值,和/或减小θ1/θ2的比值,和/或增大d1/d2的比值,和/或减小h3/h1的比值,和/或减小θ1/θ3的比值,和/或增大w值,进而使坯料7更易流向翼片型腔10;若坯料7充满主型腔9的速度小于充满翼片型腔10的速度,则减小L1/L2的比值,和/或增大θ1/θ2的比值,和/或减小d1/d2的比值,和/或增大h3/h1的比值,和/或增大θ1/θ3的比值,和/或减小w值,进而使坯料7更易流向主型腔9,直至坯料7充满主型腔9和翼片型腔10的速度相等,此时成形出的工件11的金属流线将更加均匀,具有更优的各向同性和力学性能;S5, flow rate adjustment: in the process of step S3, if the speed of blank 7 filling the main cavity 9 is greater than the speed of filling the airfoil cavity 10, then increase the ratio of L1/L2, and/or reduce the ratio of θ1/θ2 , and/or increase the ratio of d1/d2, and/or reduce the ratio of h3/h1, and/or reduce the ratio of θ1/θ3, and/or increase the value of w, thereby making the blank 7 more likely to flow to the fin Cavity 10; if the blank 7 fills the main cavity 9 at a lower speed than the airfoil cavity 10, then reduce the ratio of L1/L2, and/or increase the ratio of θ1/θ2, and/or decrease d1 /d2 ratio, and/or increase the ratio of h3/h1, and/or increase the ratio of θ1/θ3, and/or reduce the w value, so that the blank 7 can flow to the main cavity 9 more easily until the blank 7 is full The speeds of the main cavity 9 and the vane cavity 10 are equal, and the metal streamline of the formed workpiece 11 will be more uniform at this time, and have better isotropy and mechanical properties;
S6、重复步骤S2至S4,直至成形出预定数量的工件11。S6. Steps S2 to S4 are repeated until a predetermined number of
优选地实施例中,所述挤压面8呈中间高四周低或中间低四周高的锥形面;当所述挤压面8呈中间高四周低的锥形面时,若坯料7充满主型腔9的速度大于充满翼片型腔10的速度,则增大挤压面8中部的凸起高度,若坯料7充满主型腔9的速度小于充满翼片型腔10的速度,则减小挤压面8中部的凸起高度;当所述挤压面8呈中间低四周高的锥形面时,若坯料7充满主型腔9的速度大于充满翼片型腔10的速度,则减小挤压面8中部的下凹的深度,若坯料7充满主型腔9的速度小于充满翼片型腔10的速度,则增大挤压面8中部的下凹的深度。In a preferred embodiment, the
以上所述仅为本发明的较佳实施例,并非对本案设计的限制,凡依本案的设计关键所做的等同变化,均落入本案的保护范围。The above descriptions are only preferred embodiments of the present invention, and are not limitations on the design of this case. All equivalent changes made according to the design key of this case all fall within the scope of protection of this case.
Claims (10)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211221359.2A CN115488181B (en) | 2022-10-08 | 2022-10-08 | Even extrusion forming mould of magnalium section bar |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202211221359.2A CN115488181B (en) | 2022-10-08 | 2022-10-08 | Even extrusion forming mould of magnalium section bar |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN115488181A true CN115488181A (en) | 2022-12-20 |
| CN115488181B CN115488181B (en) | 2025-07-18 |
Family
ID=84473376
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202211221359.2A Active CN115488181B (en) | 2022-10-08 | 2022-10-08 | Even extrusion forming mould of magnalium section bar |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN115488181B (en) |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH105850A (en) * | 1996-06-19 | 1998-01-13 | Sumitomo Light Metal Ind Ltd | Extrusion dies |
| JPH11285727A (en) * | 1998-03-31 | 1999-10-19 | Showa Alum Corp | Extrusion manufacturing method of clad material |
| JP2002172420A (en) * | 2000-12-01 | 2002-06-18 | Showa Denko Kk | Die for manufacturing aluminum extruding section with fin |
| JP2012024769A (en) * | 2010-07-20 | 2012-02-09 | Showa Denko Kk | Extruding die for manufacturing half-hollow section |
| CN103521545A (en) * | 2013-07-30 | 2014-01-22 | 中北大学 | Final extrusion forming die for high-strength complicated aluminum alloy special-shape outer hexagonal base metal plate |
| CN205200198U (en) * | 2015-11-17 | 2016-05-04 | 西南铝业(集团)有限责任公司 | Alloy extrusion device and material mould is arranged in extrusion thereof |
| US20180369889A1 (en) * | 2017-06-27 | 2018-12-27 | North University Of China | Special-purpose Die for Shaping Aluminum-magnesium Alloy by Rotating Extrusion |
| CN110180911A (en) * | 2019-05-29 | 2019-08-30 | 安徽生信铝业股份有限公司 | A kind of Semi surrounding type hollow aluminum section extrusion die and preparation method thereof |
| CN110883122A (en) * | 2019-11-28 | 2020-03-17 | 中北大学 | Large-size and large-height-diameter ratio magnesium alloy cast rods with short flow and large deformation billet making method |
| CN211613856U (en) * | 2019-12-25 | 2020-10-02 | 佛山市深达美特种铝合金有限公司 | Extrusion die for aluminum alloy seamless profile of aircraft tail |
-
2022
- 2022-10-08 CN CN202211221359.2A patent/CN115488181B/en active Active
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH105850A (en) * | 1996-06-19 | 1998-01-13 | Sumitomo Light Metal Ind Ltd | Extrusion dies |
| JPH11285727A (en) * | 1998-03-31 | 1999-10-19 | Showa Alum Corp | Extrusion manufacturing method of clad material |
| JP2002172420A (en) * | 2000-12-01 | 2002-06-18 | Showa Denko Kk | Die for manufacturing aluminum extruding section with fin |
| JP2012024769A (en) * | 2010-07-20 | 2012-02-09 | Showa Denko Kk | Extruding die for manufacturing half-hollow section |
| CN103521545A (en) * | 2013-07-30 | 2014-01-22 | 中北大学 | Final extrusion forming die for high-strength complicated aluminum alloy special-shape outer hexagonal base metal plate |
| CN205200198U (en) * | 2015-11-17 | 2016-05-04 | 西南铝业(集团)有限责任公司 | Alloy extrusion device and material mould is arranged in extrusion thereof |
| US20180369889A1 (en) * | 2017-06-27 | 2018-12-27 | North University Of China | Special-purpose Die for Shaping Aluminum-magnesium Alloy by Rotating Extrusion |
| CN110180911A (en) * | 2019-05-29 | 2019-08-30 | 安徽生信铝业股份有限公司 | A kind of Semi surrounding type hollow aluminum section extrusion die and preparation method thereof |
| CN110883122A (en) * | 2019-11-28 | 2020-03-17 | 中北大学 | Large-size and large-height-diameter ratio magnesium alloy cast rods with short flow and large deformation billet making method |
| CN211613856U (en) * | 2019-12-25 | 2020-10-02 | 佛山市深达美特种铝合金有限公司 | Extrusion die for aluminum alloy seamless profile of aircraft tail |
Non-Patent Citations (4)
| Title |
|---|
| 代昌浩等: "镁合金型材挤压过程数值模拟及模具优化设计", 热加工工艺, no. 11, 6 June 2018 (2018-06-06), pages 178 - 180 * |
| 程眉等: "多向塑性成形数值模拟研究", 锻压技术, no. 05, 25 October 2007 (2007-10-25), pages 129 - 132 * |
| 苏丽旭: "基于镁合金挤压成形及复合模具研究设计", 农业装备技术, vol. 48, no. 230, 10 August 2022 (2022-08-10), pages 42 - 44 * |
| 苗站等: "不同参数对铝合金枝杈类构件金属流线的影响及优化", 锻压技术, vol. 46, no. 2, 19 February 2021 (2021-02-19), pages 105 - 110 * |
Also Published As
| Publication number | Publication date |
|---|---|
| CN115488181B (en) | 2025-07-18 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN110695112B (en) | Radial-reverse combined extrusion forming method for thin-walled cylindrical part with outer boss | |
| JP3663413B2 (en) | Method for producing thin metal plate having a large number of projections on the surface | |
| CN110918844A (en) | A spatial envelope forming method for thin-walled, multi-ring, high-rib members | |
| CN103350178B (en) | The slide-and-lock device of valve body forging mold | |
| CN110695111A (en) | Radial-reverse combined extrusion forming die for thin-walled cylindrical part with outer boss | |
| CN116422820A (en) | A two-direction closed die forging method for thin-walled deep-hole gear forgings | |
| CN115283471B (en) | A Method of Forward Extrusion Uniform Forming for Complicated Profiles | |
| CN111889531B (en) | Positive and negative extrusion forming die and forming method for curved bus type shell | |
| WO2018221497A1 (en) | Powder molding press method of green compact for cutting insert, and powder molding press device | |
| CN112139424A (en) | Cylindrical part plate forging forming die with small round corner characteristic and method | |
| CN115488181A (en) | Uniform extrusion forming die for magnesium-aluminum alloy section | |
| CN102581056A (en) | Die and method for machining sleeve part with steps in inner hole | |
| CN113600634B (en) | Extrusion forming method of cylindrical part with boss | |
| CN213195473U (en) | Die for closed precision forging of Y-shaped cylinder of revolution | |
| CN206169144U (en) | Pressure forming device | |
| CN111014553B (en) | Forging method for controlling size angle of irregular triangular rough shape | |
| CN115351215A (en) | Accurate forming die of eccentric water droplet type end cover forging along with shape | |
| WO2018090989A1 (en) | Pressure forming device and pressure forming method | |
| CN204657379U (en) | Permeability type shaft member cold closed-die forging mould | |
| CN218171206U (en) | Multi-workpiece rapid injection mold | |
| CN222902535U (en) | A planet carrier forging die | |
| CN206527174U (en) | A kind of closed type extrusion molding dies of differential gear | |
| CN207103458U (en) | A kind of cold-extrusion shaping mould of oil pump cover plate | |
| US2571520A (en) | Method of making bullets | |
| CN222830630U (en) | Conical tooth forging die |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |
