CN115652047A - A slotted mandrel extrusion strengthening process to improve the uniformity of residual stress around the hole - Google Patents
A slotted mandrel extrusion strengthening process to improve the uniformity of residual stress around the hole Download PDFInfo
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Abstract
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技术领域technical field
本发明涉及一种开缝芯棒两次挤压强化的孔周残余应力均匀化的孔挤压强化方法,属于孔挤压强化的抗疲劳制造技术领域,尤其涉及采用开缝芯棒对带孔试样进行两次方向相反的挤压强化。The invention relates to a hole extrusion strengthening method for uniformizing the residual stress around the hole by twice extrusion strengthening of a slotted mandrel, which belongs to the field of anti-fatigue manufacturing technology of hole extrusion strengthening, and particularly relates to the use of a slotted mandrel to The samples were strengthened by extrusion twice in opposite directions.
背景技术Background technique
连接孔是飞机上较多的连接结构,通过在连接孔中安装紧固件将飞机结构之间进行相互连接,由于连接孔的存在,导致材料不连续,带孔试样在承受外加交变载荷作用下易于萌生疲劳裂纹,影响带孔试样的疲劳寿命。孔挤压强化是抗疲劳制造技术中简单有效的工艺,在航空领域应用广泛。然而,采用开缝衬套、实心芯棒对带孔试样进行孔挤压强化,挤压强化后试样孔壁形成不均匀的残余压应力,影响带孔试样的疲劳性能。Connecting holes are more connecting structures on aircraft. Fasteners are installed in connecting holes to connect aircraft structures. Due to the existence of connecting holes, the material is discontinuous, and the sample with holes is subjected to external alternating loads. Fatigue cracks are easy to initiate under the action, which affects the fatigue life of the sample with holes. Hole extrusion strengthening is a simple and effective process in anti-fatigue manufacturing technology, and it is widely used in the aerospace field. However, when the slotted bushing and solid mandrel are used to strengthen the hole by extrusion, the hole wall of the sample will form uneven residual compressive stress after extrusion strengthening, which will affect the fatigue performance of the hole.
公开号为CN111118270B的中国专利文件(下文简称文件1),提出了孔周残余应力均匀化冷挤压工艺和装置,该孔周残余应力均匀化冷挤压工艺,适用于直通孔,该冷挤压工艺包括通过第一芯棒沿第一轴向对直通孔进行第一次强化;通过第二芯棒沿第二轴向对直通孔进行第二次强化;其中,第一轴向与第二轴向相反,第一芯棒的进行强化部分的最大直径小于或等于第二芯棒的进行强化部分的最大直径。采用两步双向冷挤压强化后,直通孔的周向残余应力沿厚度方向分布更为均匀,且在两个端面的孔边均未产生残余拉应力,对提高强化孔的抗疲劳性能有利。该专利文件与本申请文件的主要区别:(1)孔挤压强化工具不同。文件1使用的孔挤压强化工具为衬套,且先后两次孔挤压强化使用的衬套厚度不同,而本申请中使用孔挤压强化工具为开缝芯棒,且两次孔挤压强化使用的开缝芯棒相同,降低了工艺成本。(2)孔挤压强化工艺。本申请中提到的开缝芯棒两次挤压强化,第二次挤压强化时需要将开缝芯棒旋转一定角度,目的是去除开缝芯棒第一次挤压强化时带孔试样孔壁形成的凸脊,孔周残余应力均匀化冷挤压工艺和装置专利文件对挤压芯棒的角度未限制。(3)铰削加工。本申请采用开缝芯棒进行两次挤压强化,需要进行铰削加工对挤压强化后的试样孔壁进行修整,目的使孔挤压强化后试样孔径达到终孔直径,文件1中未提到两次挤压强化后需要进行铰削加工。。The Chinese patent document with the publication number CN111118270B (hereinafter referred to as Document 1) proposes a cold extrusion process and device for uniform residual stress around the hole. The cold extrusion process for uniform residual stress around the hole is suitable for straight through holes. The pressing process includes the first strengthening of the through hole along the first axis through the first mandrel; the second strengthening of the through hole along the second axis through the second mandrel; wherein, the first axis and the second Axially opposite, the maximum diameter of the portion of the first mandrel to be strengthened is less than or equal to the maximum diameter of the portion of the second mandrel to be strengthened. After strengthening by two-step bidirectional cold extrusion, the circumferential residual stress of the through hole is distributed more uniformly along the thickness direction, and no residual tensile stress occurs at the edge of the hole on the two end faces, which is beneficial to improving the fatigue resistance of the strengthened hole. The main differences between this patent document and this application document: (1) The hole extrusion strengthening tools are different. The hole extrusion strengthening tool used in
公开号为:CN114085968A的中国专利文件(下文简称文件2),提出了一种开缝衬套冷挤压装配孔强化方法及配套工装装置,方法包括:步骤S1-S5。配套工装包括挤压枪、挤压芯棒和衬套顶块;外壳体内设置有活塞腔,活塞腔内设置有伸缩活动机构,外壳体的前端设置有伸长端,伸长端内开设有与活塞腔连通的伸缩通道,伸缩通道内设置有伸缩杆,伸缩杆的一端与伸缩活动机构连接;挤压芯棒的端部设置有环形的第一挤压部,第一挤压部与第二挤压部之间设置有放置开缝衬套的过渡段;衬套顶块为上大下小的锥形管状结构,衬套顶块套在挤压芯棒上。其提出了利用开缝衬套对装配孔进行二次挤压强化的方法,实现整个装配孔应力值的均匀性,更好地保证强化质量和效果,进一步显著提高抗疲劳性能。该专利文件2与本申请文件的主要区别:(1)挤压强化工具。文件2中使用的孔挤压强化工具为开缝衬套,每进行一次挤压强化需要更换一个开缝衬套,而本申请文件中在带孔试样两次挤压强化过程均使用同一根芯棒。(2)孔挤压强化时挤压强化工具的开缝位置。文件2中前后两次挤压强化时使用的开缝衬套的开缝位置对齐,这样经过两次挤压强化后试样孔壁的凸脊依然存在,而本申请文件中,带孔试样进行第二次开缝芯棒孔挤压强化时开缝芯棒旋转10-30°的角度,这样可以消除开缝芯棒第一次挤压强化时带孔试样孔壁形成的凸脊。(3)挤压芯棒结构不同。文件2中第二次挤压强化时使用芯棒为实心芯棒,且实心芯棒包含两个挤压部,第一挤压部、第二挤压部,且第一挤压部的直径大于第二挤压部的直径,本申请文件中使用的挤压芯棒为开缝芯棒,挤压芯棒的挤压强化部位设置开缝,带孔试样能够实现单侧挤压强化,开缝芯棒的结构由连接段、导向段、前锥段、工作环、后锥段等组成,其中前锥段、工作环、后锥段为开缝芯棒的挤压强化部位,开缝芯棒两次挤压强化使用的芯棒为同一根开缝芯棒。(4)带孔试样两次挤压强化的形式不同。文件2中,将开缝衬套从装配孔的一端插入装配孔内,挤压工装装置驱动挤压芯棒收缩,挤压芯棒上的第一挤压部向后收缩挤压开缝衬套,第一挤压部完全抽出开缝衬套后,完成第一次挤压,将开缝衬套从装配孔中取出,更换一个新的开缝衬套装配到挤压芯棒上,将新的开缝衬套从装配孔的另一端插入装配孔内,且使用新的开衬套的开缝位置与第一次挤压使用的开缝衬套的开缝位置对齐,挤压工装装置驱动挤压芯棒收缩,挤压芯棒上的第一挤压部向后收缩挤压开缝衬套,第一挤压部完全抽出开缝衬套后,完成第二次挤压。本申请文件中,开缝芯棒正面穿过辅助板、带孔试样,匀速拉出插入支撑棒的开缝芯棒,完成带孔试样的第一次孔挤压强化,将带孔试样翻转180°,将开缝芯棒第一次孔挤压强化试样孔壁的挤入端作为开缝芯棒第二次孔挤压强化试样孔壁的挤出端,将开缝芯棒第一次孔挤压强化试样孔壁的挤出端作为开缝芯棒第二次孔挤压强化试样孔壁的挤入端,将开缝芯棒旋转10°~30°,对开缝芯棒的挤压强化部位施加力,使开缝芯棒挤压强化部位的开缝发生收缩,开缝芯棒能够正面穿过辅助板、开缝芯棒第一次孔挤压强化试样,在开缝芯棒中插入支撑棒,匀速拉出插入支撑棒的开缝芯棒,带孔试样完成开缝芯棒第二次孔挤压强化。The Chinese patent document with the publication number CN114085968A (hereinafter referred to as document 2) proposes a method for strengthening the cold extrusion assembly hole of a slotted bush and a supporting tooling device. The method includes steps S1-S5. The matching tooling includes an extrusion gun, an extrusion mandrel and a bushing top block; a piston chamber is arranged in the outer casing, a telescopic movable mechanism is arranged in the piston chamber, and an extension end is arranged at the front end of the outer casing, and an extension end is provided in the extension end. A telescopic passage connected to the piston cavity, a telescopic rod is arranged in the telescopic passage, and one end of the telescopic rod is connected with the telescopic movable mechanism; the end of the extruding mandrel is provided with an annular first extrusion part, and the first extrusion part is connected to the second A transition section for placing slotted bushes is arranged between the extrusion parts; the bushing top block is a conical tubular structure with a large upper part and a smaller bottom part, and the bushing top block is set on the extrusion mandrel. It proposes a method of secondary extrusion strengthening of the assembly hole by using a slotted bush to achieve the uniformity of the stress value of the entire assembly hole, better ensure the quality and effect of strengthening, and further significantly improve the fatigue resistance. The main differences between this
综上所述,孔挤压强化技术中开缝衬套、实心芯棒应用较广泛,然而开缝衬套壁薄,孔挤压强化过程中易于发生大的塑性变形,导致开缝衬套不能进行重复使用,严重影响开缝芯棒孔挤压强化工艺成本,而实心芯棒的挤压强化部位直径大于带孔试样初孔直径,导致实心芯棒孔挤压强化工艺应用范围存在局限性。结合开缝衬套与实心芯棒,提出的开缝芯棒孔挤压强化工艺能够解决开缝衬套、实心芯棒存在的问题。但采用开缝芯棒对带孔试样进行一次挤压强化,孔挤压强化后试样孔壁挤入端、中间层、挤出端等位置承受的挤压力不同,试样孔壁发生的塑性变形程度不同,导致带孔试样孔挤压强化后试样孔壁形成不均匀的残余压应力。为此,本发明提出一种提升孔周残余应力均匀化程度的开缝芯棒挤压强化工艺,旨在实现开缝芯棒两次挤压强化后带孔试样孔壁形成均匀的残余压应力,提高带孔试样的疲劳性能。In summary, slotted bushings and solid mandrels are widely used in hole extrusion strengthening technology. However, the wall of slotted bushings is thin, and large plastic deformation is prone to occur in the process of hole extrusion strengthening, resulting in the failure of slotted bushings. Repeated use will seriously affect the cost of the extrusion strengthening process of the slotted mandrel hole, and the diameter of the extrusion strengthening part of the solid mandrel is larger than the diameter of the initial hole of the sample with holes, resulting in limitations in the application range of the extrusion strengthening process of the solid mandrel hole . Combining the slotted bushing and the solid mandrel, the hole extrusion strengthening process of the slotted mandrel can solve the existing problems of the slotted bushing and the solid mandrel. However, the slotted mandrel is used to squeeze and strengthen the sample with a hole once. After the hole is squeezed and strengthened, the extrusion force on the extrusion end, the middle layer, and the extrusion end of the sample hole wall is different, and the sample hole wall occurs. The degree of plastic deformation of the sample with holes is different, resulting in the formation of non-uniform residual compressive stress on the wall of the sample hole after the hole is squeezed and strengthened. For this reason, the present invention proposes a slotted mandrel extrusion strengthening process to improve the uniformity of the residual stress around the hole, aiming at forming a uniform residual pressure on the hole wall of the sample with holes after two times of extrusion strengthening of the slotted mandrel. Stress, improve the fatigue performance of the sample with holes.
发明内容Contents of the invention
针对上述采用开缝衬套对带孔试样进行孔挤压强化过程中挤压芯棒挤压开缝衬套,开缝衬套发生弹性变形挤压带孔试样孔壁。由于开缝衬套壁薄,孔挤压强化过程中开缝衬套易于发生大的塑性变形,导致开缝衬套不能进行二次挤压强化,增加了工艺成本。若采用实心芯棒对带孔试样进行孔挤压强化,实心芯棒工作环直径大于带孔试样初孔直径,实心芯棒从芯棒挤压强化部位穿过带孔试样,即不能实现带孔试样单边挤压强化,导致实心芯棒不能进行大型带孔试样的挤压强化,存在工艺局限性。In view of the above-mentioned process of using the slotted bushing to squeeze the holed sample to strengthen the hole, the extrusion mandrel squeezes the slotted bushing, and the slotted bushing elastically deforms and squeezes the wall of the holed sample. Due to the thin wall of the slotted bushing, the slotted bushing is prone to large plastic deformation during the hole extrusion strengthening process, so that the slotted bushing cannot be strengthened by secondary extrusion, which increases the process cost. If a solid mandrel is used to carry out hole extrusion strengthening on the sample with holes, the diameter of the working ring of the solid mandrel is larger than the diameter of the initial hole of the sample with holes, and the solid mandrel passes through the sample with holes from the extrusion strengthening part of the mandrel, that is, it cannot The realization of unilateral extrusion strengthening of the sample with holes leads to the fact that the solid mandrel cannot be used for extrusion strengthening of large samples with holes, and there are technological limitations.
基于开缝衬套、实心芯棒,提出了开缝芯棒孔挤压强化工艺。开缝芯棒挤压强化部位存在开缝,孔挤压强化前,对开缝芯棒挤压强化部位施加力,开缝芯棒挤压强化部位的开缝发生收缩,开缝芯棒工作环直径小于试样初孔直径,开缝芯棒能够从挤压强化部位穿过带孔试样,实现带孔试样的单侧挤压强化。开缝芯棒孔挤压强化过程中,试样孔壁挤入端、挤出端不受约束为自由端,孔壁中间层受到挤入端、挤出端的约束,孔壁中间层承受的挤压力大于挤入端、挤出端,开缝芯棒沿带孔试样孔壁发生轴向反向的运动,孔壁材料受到挤压力作用发生沿试样孔壁轴向方向的金属流动,引起试样孔壁挤入端的挤压量小,试样孔壁挤出端的挤压量大。因此,孔壁中间层的塑性变形程度>孔壁挤出端的塑性变形程度>孔壁挤入端的塑性变形程度,引起孔壁中间层的残余压应力>孔壁挤出端的残余压应力>孔壁挤入端的残余压应力。针对开缝芯棒孔挤压强化后带孔试样孔壁形成不均匀的残余压应力,本发明提出了一种提升孔周残余应力均匀化程度的开缝芯棒挤压强化工艺,使用该发明对带孔试样进行方向相反的两次孔挤压强化,试样孔壁挤入端、挤出端塑性变形程度较均匀,孔壁形成的残余压应力较均匀,从而能够提高带孔试样的疲劳性能。Based on slotted bushing and solid mandrel, a slotted mandrel hole extrusion strengthening process is proposed. There is a slit in the extrusion strengthening part of the slotted mandrel. Before the hole extrusion strengthening, a force is applied to the extrusion strengthening part of the slotted mandrel. The slot in the extrusion strengthening part of the slotted mandrel shrinks, and the working ring of the slotted mandrel The diameter is smaller than the diameter of the initial hole of the sample, and the slotted mandrel can pass through the sample with a hole from the extrusion strengthening part to realize the unilateral extrusion strengthening of the sample with a hole. During the extrusion strengthening process of the slotted mandrel hole, the extrusion end and extrusion end of the sample hole wall are not constrained to be free ends, the middle layer of the hole wall is constrained by the extrusion end and extrusion end, and the extrusion force borne by the middle layer of the hole wall is The pressure is greater than the extrusion end and the extrusion end, and the slotted mandrel moves axially and reversely along the hole wall of the sample hole, and the material of the hole wall is subjected to the extrusion force to produce metal flow along the axial direction of the sample hole wall , resulting in a small amount of extrusion at the inlet end of the sample hole wall, and a large extrusion amount at the extrusion end of the sample hole wall. Therefore, the plastic deformation degree of the middle layer of the hole wall > the plastic deformation degree of the extrusion end of the hole wall > the plastic deformation degree of the extrusion end of the hole wall, resulting in the residual compressive stress of the middle layer of the hole wall > the residual compressive stress of the hole wall extrusion end > the hole wall Residual compressive stress at the extrusion end. Aiming at the inhomogeneous residual compressive stress formed on the hole wall of the sample with holes after extrusion strengthening of the slotted mandrel hole, the present invention proposes a slotted mandrel extrusion strengthening process to improve the uniformity of the residual stress around the hole. The invention carries out two times of hole extrusion strengthening in opposite directions to the sample with holes, the degree of plastic deformation of the sample hole wall at the extrusion end and the extrusion end is relatively uniform, and the residual compressive stress formed on the hole wall is relatively uniform, so that the test with holes can be improved. Such fatigue performance.
技术方案:为了实现上述发明目的,本发明采用了以下技术方案:Technical solution: In order to realize the above invention object, the present invention adopts the following technical solutions:
提升孔周残余应力均匀化程度的开缝芯棒挤压强化工艺,包括以下步骤:The slotted mandrel extrusion strengthening process to improve the uniformity of the residual stress around the hole includes the following steps:
(1)带孔试样安装。开缝芯棒挤压强化段存在开缝,孔挤压强化前对开缝芯棒挤压强化段施加力,开缝芯棒挤压强化段的开缝发生收缩,开缝芯棒工作环直径小于带孔试样初孔直径,开缝芯棒可以从挤压强化段依次穿过辅助板、带孔试样,辅助板、带孔试样放置于开缝芯棒导向段,且带孔试样安装过程中开缝芯棒不对试样孔壁进行挤压强化;(1) Install the sample with holes. There is a slit in the extrusion strengthening section of the slotted mandrel, and force is applied to the extrusion strengthening section of the slotted mandrel before the hole extrusion strengthening, the slit of the extrusion strengthening section of the slotted mandrel shrinks, and the diameter of the working ring of the slotted mandrel Smaller than the diameter of the initial hole of the sample with a hole, the slotted mandrel can pass through the auxiliary plate and the sample with a hole in sequence from the extrusion strengthening section, and the auxiliary plate and the sample with a hole are placed in the guide section of the slotted mandrel, and the test piece with a hole During the sample installation process, the slotted mandrel does not squeeze and strengthen the sample hole wall;
(2)安装支撑棒。在开缝芯棒依次穿过辅助板、带孔试样的同一侧,向开缝芯棒中插入支撑棒,支撑棒的支撑作用,开缝芯棒挤压强化段不发生收缩,开缝芯棒的工作环直径大于带孔试样初孔直径;(2) Install the support rod. When the slotted mandrel passes through the auxiliary plate and the same side of the sample with holes in turn, a support rod is inserted into the slotted mandrel. With the support function of the support rod, the slotted mandrel extrudes the strengthening section without shrinkage, and the slotted mandrel does not shrink. The diameter of the working ring of the rod is greater than the diameter of the initial hole of the sample with holes;
(3)带孔试样一次孔挤压强化。从带孔试样中匀速拉出插入支撑棒的开缝芯棒,开缝芯棒与带孔试样孔壁直接接触,开缝芯棒挤压强化试样孔壁,孔壁材料发生弹塑性变形,孔壁形成有益的残余压应力,完成带孔试样的一次挤压强化;(3) One-time hole extrusion strengthening of the sample with holes. Pull out the slotted mandrel inserted into the support rod from the sample with holes at a uniform speed, the slotted mandrel is in direct contact with the hole wall of the sample with holes, the slotted mandrel squeezes and strengthens the hole wall of the sample, and the material of the hole wall becomes elastic-plastic Deformation, the hole wall forms beneficial residual compressive stress, and completes the primary extrusion strengthening of the sample with holes;
(4)开缝芯棒两次挤压强化。由于开缝芯棒的挤压强化段存在开缝,开缝芯棒孔挤压强化后试样孔壁形成凸脊,凸脊影响试样孔壁质量,凸脊根部易于萌生疲劳裂纹。因此,开缝芯棒孔挤压强化后需要进行铰削加工。但开缝芯棒孔挤压强化过程中,带孔试样挤入端、挤出端不受约束为自由端,试样孔壁中间层受到挤入端、挤出端的约束,试样中间层受到的挤压力大于孔壁挤入端、挤出端,开缝芯棒沿带孔试样轴向方向运动过程中,孔壁材料沿轴向方向发生金属流动,引起孔壁挤入端的实际挤压量小,孔壁挤出端的实际挤压量大,则开缝芯棒孔挤压强化后试样孔壁挤入端形成的残余压应力<试样孔壁挤出端形成的残余压应力<试样孔壁中间层形成的残余压应力。因此,采用开缝芯棒对带孔试样进行两次挤压强化,增加带孔试样孔壁材料的塑性变形程度,增大带孔试样孔壁残余压应力。(4) Slotted mandrel is extruded twice to strengthen. Due to the slits in the extrusion strengthening section of the slotted mandrel, the hole wall of the sample hole after extrusion strengthening of the slotted mandrel forms a ridge, which affects the quality of the sample hole wall, and the root of the ridge is prone to fatigue cracks. Therefore, the slotted mandrel hole needs to be reamed after extrusion strengthening. However, during the extrusion strengthening process of the slotted mandrel hole, the intrusion end and extrusion end of the sample with holes are not constrained to be free ends, the middle layer of the sample hole wall is constrained by the intrusion end and extrusion end, and the middle layer of the sample The extrusion force received is greater than the extrusion end and extrusion end of the hole wall. During the movement of the slotted mandrel along the axial direction of the sample with holes, the metal flow of the hole wall material along the axial direction will cause the actual deformation of the hole wall extrusion end. If the extrusion amount is small and the actual extrusion amount at the extrusion end of the hole wall is large, then the residual compressive stress formed at the extrusion end of the sample hole wall after the extrusion strengthening of the slotted mandrel hole is smaller than the residual compressive stress formed at the extrusion end of the sample hole wall Stress <The residual compressive stress formed by the middle layer of the sample hole wall. Therefore, the perforated sample is extruded twice to strengthen the sample with a slotted mandrel to increase the degree of plastic deformation of the hole wall material of the holed sample and increase the residual compressive stress of the hole wall of the holed sample.
所述的“开缝芯棒两次挤压强化”是开缝芯棒一次挤压强化+开缝芯棒旋转一定角度异向两次挤压强化,所述的“旋转一定角度”是把开缝芯棒旋转10°~30°。The "twice extrusion strengthening of the slotted mandrel" is one extrusion strengthening of the slotted mandrel + two times of extrusion strengthening of the slotted mandrel rotating at a certain angle in different directions, and the "rotating at a certain angle" is the The sewing mandrel rotates 10°~30°.
上述“开缝芯棒两次孔挤压强化工艺”优选:The above-mentioned "slotted mandrel double-hole extrusion strengthening process" is preferred:
(1)方案:(1) Scheme:
方案1:开缝芯棒同向两次挤强化,其中,第二次孔挤压强化的方向与第一次孔挤压强化的方向相同。Scheme 1: Slotted mandrel double extrusion strengthening in the same direction, wherein the direction of the second hole extrusion strengthening is the same as that of the first hole extrusion strengthening.
方案2:开缝芯棒异向两次挤压强化,其中,第二次孔挤压强化的方向与第一次孔挤压强化的方向相反。Scheme 2: The slotted mandrel is strengthened by double extrusion in different directions, wherein the direction of the second hole extrusion strengthening is opposite to that of the first hole extrusion strengthening.
方案3:开缝芯棒一次挤压强化+开缝芯棒旋转一定角度同向两次挤压强化,是在方案1的基础上,开缝芯棒进行第二次孔挤压强化时开缝芯棒旋转一定角度。Scheme 3: Slotted mandrel one-time extrusion strengthening + slotted mandrel rotation at a certain angle and two extrusion strengthenings in the same direction, based on
方案4:开缝芯棒一次挤压强化+开缝芯棒旋转一定角度异向两次挤压强化,是在方案3的基础上,开缝芯棒进行第二次孔挤压强化时开缝芯棒旋转一定角度。Scheme 4: Slotted mandrel one-time extrusion strengthening + slotted mandrel rotated at a certain angle and two extrusions in different directions to strengthen, it is based on
其中方案3、方案4的“旋转一定角度”是指“开缝芯棒旋转10°~30°”。Among them, the "rotation by a certain angle" in
(2)结果与结论分析:(2) Results and conclusion analysis:
其中,方案1(开缝芯棒同向两次挤压强化),不能消除一次挤压强化后孔壁形成的凸脊,且会增加孔壁形成凸脊的高度,由于孔壁进行了两次挤压强化,挤压强化后孔壁材料塑性变形程度大于开缝芯棒一次挤压强化,孔壁形成的残余压应力大于开缝芯棒一次挤压强化。Among them, scheme 1 (slotted mandrel double extrusion strengthening in the same direction) cannot eliminate the ridges formed on the hole wall after one extrusion strengthening, and will increase the height of the ridges formed on the hole wall, because the hole wall has been strengthened twice Extrusion strengthening, the degree of plastic deformation of the hole wall material after extrusion strengthening is greater than that of the slotted mandrel for one-time extrusion strengthening, and the residual compressive stress formed by the hole wall is greater than that of the slotted mandrel for one-time extrusion strengthening.
方案2(开缝芯棒异向两次挤压强化),第一次孔挤压强化试样孔壁的挤入端(挤出端)是第二次孔挤压强化试样的挤出端(挤入端),该方案不能消除开缝芯棒一次挤压强化孔壁形成的凸脊,且增加孔壁形成凸脊的高度,由于孔壁进行了两次挤压强化,挤压强化后孔壁材料塑性变形程度大于开缝芯棒一次挤压强化,孔壁形成的残余压应力大于开缝芯棒一次挤压强化,开缝芯棒两次异向孔挤压强化后,试样孔壁形成的残余压应力较均匀。Scheme 2 (slotted mandrel double extrusion strengthening), the extrusion end (extrusion end) of the hole wall of the first hole extrusion strengthening sample is the extrusion end of the second hole extrusion strengthening sample (extrusion end), this scheme cannot eliminate the ridge formed by one-time extrusion of the slotted mandrel to strengthen the hole wall, and increase the height of the ridge formed by the hole wall. Since the hole wall has been extruded twice, after extrusion The degree of plastic deformation of the hole wall material is greater than that of the slotted mandrel for one-time extrusion strengthening, and the residual compressive stress formed by the hole wall is greater than that of the slotted mandrel for one-time extrusion strengthening. The residual compressive stress formed by the wall is relatively uniform.
方案3(开缝芯棒一次挤压强化+开缝芯棒旋转一定角度同向两次挤压强化),第二次孔挤压强化可以消除开缝芯棒一次挤压强化时孔壁形成的凸脊,增加了试样孔壁材料的塑性变形程度,孔挤压强化后孔壁材料塑性变形程度大于开芯棒一次挤压强化,孔壁形成的残余压应力大于开缝芯棒一次挤压强化。Scheme 3 (one-time extrusion strengthening of the slotted mandrel + two times of extrusion strengthening of the slotted mandrel in the same direction at a certain angle), the second hole extrusion strengthening can eliminate the hole wall formed by the first extrusion strengthening of the slotted mandrel The raised ridge increases the degree of plastic deformation of the hole wall material of the sample. The degree of plastic deformation of the hole wall material after the hole extrusion strengthening is greater than that of the open mandrel for one-time extrusion strengthening, and the residual compressive stress formed by the hole wall is greater than that of the slotted mandrel for one-time extrusion. strengthen.
方案4(开缝芯棒一次挤压强化+开缝芯棒旋转一定角度异向两次挤压强化),第二次孔挤压强化可以消除开缝芯棒一次挤压强化时孔壁形成的凸脊,增加了试样孔壁材料的塑性变形程度,孔挤压强化后孔壁材料塑性变形程度大于开芯棒一次挤压强化,孔壁形成的残余压应力大于开缝芯棒一次挤压强化,两次挤压强化带孔试样的方向相反,孔挤压强化后试样孔壁形成的残余应力较均匀。Scheme 4 (one-time extrusion strengthening of the slotted mandrel + two times of extrusion strengthening of the slotted mandrel in different directions at a certain angle), the second hole extrusion strengthening can eliminate the hole wall formed by the first extrusion strengthening of the slotted mandrel The raised ridge increases the degree of plastic deformation of the hole wall material of the sample. The degree of plastic deformation of the hole wall material after the hole extrusion strengthening is greater than that of the open mandrel for one-time extrusion strengthening, and the residual compressive stress formed by the hole wall is greater than that of the slotted mandrel for one-time extrusion. Strengthening, the direction of the two times of extrusion strengthening of the sample with holes is opposite, and the residual stress formed on the wall of the sample hole after hole extrusion strengthening is relatively uniform.
整体来说,方案3“开缝芯棒一次挤压强化+开缝芯棒旋转一定角度同向两次挤压强化”和方案4“开缝芯棒一次挤压强化+开缝芯棒旋转一定角度异向两次挤压强化”,两种工艺的孔挤压强化效果显著于方案1“开缝芯棒同向两次挤强化”和方案2“开缝芯棒异向两次挤压强化”。其中,方案4挤压强化后试样孔壁挤入端、挤出端孔壁形成的残余应力较均匀,孔挤压强化效果优于方案3。由于开缝芯棒挤压强化部位存在开缝,开缝芯棒孔挤压强化后试样孔壁形成凸脊,对带孔试样进行第二次挤压强化时,将开缝芯棒旋转10°~30°,开缝芯棒的第二次挤压强化能够消除开缝芯棒第一次挤压强化后试样孔壁形成的凸脊。On the whole,
(5)铰削加工。开缝芯棒两次挤压强化后,需要对挤压强化后的试样进行铰削加工,使试样孔径到达终孔直径。(5) Reaming processing. After the slotted mandrel is strengthened by extrusion twice, it is necessary to ream the sample after extrusion strengthening, so that the diameter of the sample hole reaches the diameter of the final hole.
有益效果 本发明提升孔周残余应力均匀化程度的开缝芯棒挤压强化工艺,具有以下优点:Beneficial effects The slotted mandrel extrusion strengthening process of the present invention improves the uniformity of the residual stress around the hole, and has the following advantages:
1. 孔壁残余应力均匀。采用开缝芯棒一次挤压强化后,将试样翻转180°,开缝芯棒第一次孔挤压强化试样的挤入端(挤出端)和开芯棒第二次孔挤压强化试样的挤出端(挤入端)互换,两次孔挤压强化方向相反,孔壁形成的残余压应力更为均匀。1. The residual stress of the hole wall is uniform. After the first extrusion of the slotted mandrel, the sample is turned over 180°, and the extrusion end (extrusion end) of the sample is strengthened by the first hole extrusion of the slotted mandrel and the second hole extrusion of the open mandrel. The extruded end (intruded end) of the strengthened sample is interchanged, the direction of the two hole extrusion strengthening is opposite, and the residual compressive stress formed on the hole wall is more uniform.
2. 开缝芯棒的第二次挤压强化前,将开缝芯棒(顺时针或者逆时针)旋转10°~30°,孔挤压强化效果最佳。孔挤压强化后,带孔试样孔壁挤入端、挤出端塑性变形程度更为均匀。2. Before the second extrusion strengthening of the slotted mandrel, rotate the slotted mandrel (clockwise or counterclockwise) by 10°~30°, the hole extrusion strengthening effect is the best. After the hole is strengthened by extrusion, the degree of plastic deformation of the hole wall of the sample with holes is more uniform at the extrusion end and the extrusion end.
3. 开缝芯棒两次孔挤压强化采用同一个开缝芯棒,不需要更换挤压强化工具,。开缝芯棒存在开缝,带孔试样孔挤压强化后试样孔壁形成凸脊;开缝芯棒孔挤压强化过程中,带孔试样孔壁挤入端、中间层、挤出端位置承受的挤压力不同,孔挤压强化后试样孔壁不均匀;开缝芯棒加工过程中存在加工误差,三种原因导致开缝芯棒孔挤压强化后试样孔径小于试样的终孔直径。使用相同的开缝芯棒对带孔试样进行第二次挤压强化,完成带孔试样的两次挤压强化。开缝芯棒两次孔挤压强化不需要更换或添加孔挤压强化工具,从而能够节省开缝芯棒孔挤压强化工艺成本。3. Slotted mandrel The same slotted mandrel is used for the two hole extrusion strengthening, and there is no need to replace the extrusion strengthening tool. There is a slit in the slotted mandrel, and the wall of the sample hole forms a convex ridge after extrusion strengthening of the sample hole with a hole; The extrusion force at the exit end position is different, and the hole wall of the sample after hole extrusion strengthening is uneven; there are processing errors in the processing of the slotted mandrel. Three reasons cause the hole diameter of the slotted mandrel hole to be smaller than The final hole diameter of the specimen. The second extrusion strengthening of the perforated sample was carried out using the same slotted mandrel to complete the two extrusion strengthening of the perforated sample. The two-time hole extrusion strengthening of the slotted mandrel does not need to replace or add hole extrusion strengthening tools, so that the cost of the hole extrusion strengthening process of the slotted mandrel can be saved.
附图说明Description of drawings
图1是开缝芯棒一次孔挤压强化过程。(a)挤压开缝芯棒的挤压强化段,使开缝芯棒的挤压强化段直径小于带孔试样初孔直径;(b)开缝芯棒正面依次穿过辅助板、带孔试样;(c)在开缝芯棒中插入支撑棒;(d)匀速拉出插入支撑棒的开缝芯棒。Fig. 1 is the strengthening process of one-time hole extrusion of slotted mandrel. (a) Extrude the extrusion strengthening section of the slotted mandrel so that the diameter of the extrusion strengthening section of the slotted mandrel is smaller than the diameter of the initial hole of the sample with holes; (b) The front of the slotted mandrel passes through the auxiliary plate, belt Hole sample; (c) Insert the support rod into the slotted mandrel; (d) Pull out the slotted mandrel inserted into the support rod at a uniform speed.
图2是开缝芯棒同向两次挤压强化(方案1)的示意图;Fig. 2 is a schematic diagram of the slotted mandrel double extrusion in the same direction (Scheme 1);
图3是开缝芯棒异向两次挤压强化(方案2)的示意图;Fig. 3 is a schematic diagram of the slotted mandrel double extrusion strengthening (Scheme 2);
图4是开缝芯棒一次挤压强化+开缝芯棒旋转一定角度同向两次挤压强化(方案3)的示意图。(a)开缝芯棒一次挤压强化;(b)开缝芯棒旋转一定角度的第二次同向挤压强化。Figure 4 is a schematic diagram of one-time extrusion strengthening of the slotted mandrel + double extrusion strengthening of the slotted mandrel at a certain angle in the same direction (Scheme 3). (a) Slotted mandrel primary extrusion strengthening; (b) Slotted mandrel rotated at a certain angle for the second co-extrusion strengthening.
图5是开缝芯棒一次挤压强化+开芯棒旋转一定角度异向两次挤压强化(方案4)的示意图。(a)~(d)为开缝芯棒一次孔挤压强化过程;(e)开缝芯棒第一次挤压强化后试样翻转180°;(f)开缝芯棒旋转一定角度的第二次异向挤压强化。Figure 5 is a schematic diagram of one-time extrusion strengthening of the slotted mandrel + double extrusion strengthening of the open mandrel rotating at a certain angle in different directions (Scheme 4). (a)-(d) are the one-time extrusion strengthening process of the slotted mandrel; (e) the sample is turned 180° after the first extrusion strengthening of the slotted mandrel; (f) the rotation of the slotted mandrel at a certain angle The second anisotropic extrusion strengthening.
图6是开缝芯棒孔挤压强化试样孔壁挤入端残余应力分布规律。Figure 6 shows the distribution of residual stress at the extrusion end of the hole wall of the slotted mandrel hole extrusion strengthened sample.
曲线1为开缝芯棒一次挤压强化;
曲线2为开缝芯棒一次挤压强化+开缝芯棒旋转一定角度同向两次挤压强化(方案3);
曲线3为开缝芯棒一次挤压强化+开芯棒旋转一定角度异向两次挤压强化(方案4)。
图7是开缝芯棒孔挤压强化试样孔壁中间层残余应力分布规律。Figure 7 shows the distribution of residual stress in the middle layer of the hole wall of the slotted mandrel hole extrusion strengthened sample.
曲线1为开缝芯棒一次挤压强化;
曲线2为开缝芯棒一次挤压强化+开缝芯棒旋转一定角度同向两次挤压强化(方案3);
曲线3为开缝芯棒一次挤压强化+开芯棒旋转一定角度异向两次挤压强化(方案4)。
图8是开缝芯棒孔挤压强化试样孔壁挤出端残余应力分布规律。Figure 8 shows the distribution of residual stress at the extrusion end of the hole wall of the slotted mandrel hole extrusion strengthened sample.
曲线1为开缝芯棒一次挤压强化;
曲线2为开缝芯棒一次挤压强化+开缝芯棒旋转一定角度同向两次挤压强化(方案3);
曲线3为开缝芯棒一次挤压强化+开芯棒旋转一定角度异向两次挤压强化(方案4)。
其中,1-连接段;2-导向段;3-前锥段;4-工作环;5-后锥段;6-辅助板;7-带孔试样;8-支撑棒;9-开缝芯棒一次挤压强化试样;10-开缝芯棒同向第二次挤压强化试样;11-开缝芯棒第一次挤压强化后试样翻转180°;12-开缝芯棒第一次挤压强化后试样孔壁挤入端;13-开缝芯棒第一次挤压强化后试样孔壁中间层;14-开缝芯棒第一次挤压强化后试样孔壁挤出端。Among them, 1-connection section; 2-guiding section; 3-front cone section; 4-working ring; 5-back cone section; 6-auxiliary plate; 7-sample with hole; 8-support rod; 9-slit 1st-extrusion strengthened sample of mandrel; 10-sample strengthened by second extrusion of slotted mandrel in the same direction; 11-sample turned 180° after first extrusion strengthening of slotted mandrel; 12-slotted core 13-The middle layer of the sample hole wall after the first extrusion strengthening of the slotted mandrel; 14-The test piece after the first extrusion strengthening of the slotted mandrel Extrusion end of sample hole wall.
具体实施方式Detailed ways
下面将结合附图和实施例对本发明做进一步详细说明。The present invention will be described in further detail below in conjunction with the accompanying drawings and embodiments.
实施例1 开缝芯棒孔挤压强化过程Example 1 Slotted Mandrel Hole Extrusion Strengthening Process
图1是开缝芯棒一次孔挤压强化过程。包括如下步骤:Fig. 1 is the strengthening process of one-time hole extrusion of slotted mandrel. Including the following steps:
(1)带孔试样安装。开缝芯棒挤压强化段(包括:前锥段3、工作环4、后锥段5)存在开缝,孔挤压强化前对开缝芯棒挤压强化段施加力,则开缝发生收缩,工作环4直径小于带孔试样7初孔直径,开缝芯棒从挤压强化段依次穿过辅助板6、带孔试样7后。辅助板6、带孔试样7放置于开缝芯棒导向段2,且带孔试样7安装过程中开缝芯棒不对试样孔壁进行挤压强化。(1) Install the sample with holes. Slotted mandrel extrusion strengthening section (including:
(2)安装支撑棒。从远离试样的一端向开缝芯棒中插入支撑棒-8,在支撑棒8的支撑作用下,开缝芯棒挤压强化段不发生收缩,工作环4直径大于带孔试样7初孔直径。(2) Install the support rod. Insert the support rod-8 into the slotted mandrel from the end far away from the sample. Under the support of the support rod 8, the extrusion strengthening section of the slotted mandrel does not shrink, and the diameter of the working
(3)带孔试样一次孔挤压强化。从带孔试样7中匀速拉出插入支撑棒8的开缝芯棒,开缝芯棒与带孔试样7孔壁直接接触,开缝芯棒挤压强化试样孔壁,孔壁材料发生弹塑性变形,孔壁形成有益的残余压应力,完成带孔试样的一次挤压强化。(3) One-time hole extrusion strengthening of the sample with holes. The slotted mandrel inserted into the support rod 8 is pulled out at a uniform speed from the sample with holes 7, and the slotted mandrel is in direct contact with the hole wall of the sample with holes 7, and the slotted mandrel squeezes and strengthens the hole wall of the sample, and the material of the hole wall Elastic-plastic deformation occurs, and beneficial residual compressive stress is formed on the hole wall, and the primary extrusion strengthening of the sample with holes is completed.
实施例2 开缝芯棒两次孔挤压强化工艺Example 2 Slotted mandrel double-hole extrusion strengthening process
一、方案设置:1. Program settings:
方案1:开缝芯棒同向两次挤强化,其中,第二次孔挤压强化的方向与第一次孔挤压强化的方向相同。Scheme 1: Slotted mandrel double extrusion strengthening in the same direction, wherein the direction of the second hole extrusion strengthening is the same as that of the first hole extrusion strengthening.
方案2:开缝芯棒异向两次挤压强化,其中,第二次孔挤压强化的方向与第一次孔挤压强化的方向相反。Scheme 2: The slotted mandrel is strengthened by double extrusion in different directions, wherein the direction of the second hole extrusion strengthening is opposite to that of the first hole extrusion strengthening.
方案3:开缝芯棒一次挤压强化+开缝芯棒旋转一定角度同向两次挤压强化,是在方案1的基础上,开缝芯棒进行第二次孔挤压强化时开缝芯棒旋转一定角度。Scheme 3: Slotted mandrel one-time extrusion strengthening + slotted mandrel rotation at a certain angle and two extrusion strengthenings in the same direction, based on
方案4:开缝芯棒一次挤压强化+开缝芯棒旋转一定角度异向两次挤压强化,是在方案3的基础上,开缝芯棒进行第二次孔挤压强化时开缝芯棒旋转一定角度。Scheme 4: Slotted mandrel one-time extrusion strengthening + slotted mandrel rotated at a certain angle and two extrusions in different directions to strengthen, it is based on
其中方案3、方案4的“旋转一定角度”是指“开缝芯棒旋转10°~30°”。Among them, the "rotation by a certain angle" in
二、实施过程:2. Implementation process:
图2是开缝芯棒同向两次挤压强化的示意图。按照实施例1完成带孔试样7一次挤压强化后,重复一次同样过程,实现带孔试样7的开缝芯棒同向两次挤压强化。Fig. 2 is a schematic diagram of double-extrusion strengthening of a slotted mandrel in the same direction. After the first extrusion strengthening of the sample 7 with holes was completed according to Example 1, the same process was repeated once to realize double extrusion strengthening of the slotted mandrel of the sample 7 with holes in the same direction.
图3是开缝芯棒异向两次挤压强化的示意图。按照实施例1完成带孔试样7一次挤压强化后,将得到的带孔试样翻转180°,把开缝芯棒第一次挤压强化试样孔壁的挤入端作为挤出端,把挤出端作为挤入端,重复实施例1的孔挤压强化过程,实现带孔试样7的开缝芯棒异向两次挤压强化。Fig. 3 is a schematic diagram of double-extrusion strengthening of a slotted mandrel. After completing the primary extrusion strengthening of the perforated sample 7 according to Example 1, the obtained perforated sample is turned over 180°, and the intruded end of the slotted mandrel for the first time extruded and strengthened sample hole wall is used as the extruded end , take the extrusion end as the extrusion end, repeat the hole extrusion strengthening process of Example 1, and realize the slotted mandrel of sample 7 with holes in different direction twice extrusion strengthening.
图4是开缝芯棒一次挤压强化+开缝芯棒旋转一定角度同向两次挤压强化的示意图。按照实施例1完成带孔试样7一次挤压强化后,将开缝芯棒旋转一定角度,重复实施例1的过程,实现带孔试样7的开缝芯棒一次挤压强化+开缝芯棒旋转一定角度同向两次挤压强化。Fig. 4 is a schematic diagram of one-time extrusion strengthening of the slotted mandrel + double extrusion strengthening of the slotted mandrel rotating at a certain angle in the same direction. After completing the primary extrusion strengthening of sample 7 with holes according to Example 1, rotate the slotted mandrel at a certain angle, repeat the process of Example 1, and realize the primary extrusion strengthening + slotting of the slotted mandrel of sample 7 with holes The mandrel is rotated at a certain angle and extruded twice in the same direction for strengthening.
图5是开缝芯棒一次挤压强化+开芯棒旋转一定角度异向两次挤压强化。按照实施例1完成带孔试样7一次挤压强化后,将得到的带孔试样翻转180°,把试样的挤入端作为挤出端,挤出端作为挤入端,将开缝芯棒旋转一定角度,重复实施例1的过程,可以实现带孔试样7的开缝芯棒一次挤压强化+开芯棒旋转一定角度异向两次挤压强化。Figure 5 shows the one-time extrusion strengthening of the slotted mandrel + the double-extrusion strengthening of the open mandrel rotating at a certain angle in different directions. According to Example 1, after the primary extrusion strengthening of the perforated sample 7 is completed, the obtained perforated sample is turned over 180°, the extrusion end of the sample is used as the extrusion end, and the extrusion end is used as the extrusion end. The mandrel is rotated at a certain angle, and the process of Example 1 is repeated, so that the slotted mandrel of sample 7 with a hole can be strengthened by one extrusion + the open mandrel rotated at a certain angle and twice extruded in different directions.
三、结果说明与分析3. Result description and analysis
其中,方案1、方案2,开缝芯棒的第二次孔挤压强化不能消除开缝芯棒第一次孔挤压强化过程中孔壁形成的凸脊,开缝芯棒第二次孔挤压强化后增加了开缝芯棒第一次孔挤压强化后孔壁形成的凸脊高度。因此,运用有限元仿真分析法对比方案3、方案4的孔挤压强化效果,优选出孔挤压强化效果最佳的开缝芯棒两次孔挤压强化工艺方法。Among them, in
1、通过建立开缝芯棒两次孔挤压强化三维有限元仿真分析模型,提取带孔试样孔壁挤入端、中间层、挤出端等位置的切向残余应力。开缝芯棒两次孔挤压强化带孔试样孔壁残余应力变化规律,如图6所示。1. By establishing a three-dimensional finite element simulation analysis model for two-hole extrusion strengthening of the slotted mandrel, extract the tangential residual stress at the extrusion end, middle layer, and extrusion end of the hole wall of the sample with holes. The variation law of the residual stress of the hole wall of the hole-strengthened sample with the slotted mandrel double-hole extrusion is shown in Fig. 6.
试样孔壁挤入端,方案4的孔壁形成的残余压应力大于方案3;The hole wall of the sample is squeezed into the end, and the residual compressive stress formed by the hole wall of
试样孔壁中间层,方案3、4形成的残余压应力相接近;In the middle layer of the sample hole wall, the residual compressive stress formed by
试样孔壁挤出端,方案3孔壁形成的残余压应力大于方案4。At the extrusion end of the sample hole wall, the residual compressive stress formed on the hole wall of
方案4的孔壁挤入端与挤出端形成的残余压应力较接近。The residual compressive stress formed at the extrusion end of the hole wall in
方案3的孔壁形成的残余压应力大于开缝芯棒一次挤压强化。The residual compressive stress formed by the hole wall of
2、方案1“开缝芯棒同向两次挤压强化”,带孔试样的挤压强化方向相同,开缝芯棒孔挤压强化过程中孔壁材料沿轴向方向发生金属流动,减小了试样孔壁挤入端的实际挤压量,增加了试样孔壁挤出端的实际挤压量,引起带孔试样两次同向挤压强化后试样孔壁挤出端的残余压应力大于挤入端。2.
方案2“开缝芯棒异向两次挤压强化”,带孔试样的挤压强化方向相反,开缝芯棒孔挤压强化过程中孔壁材料沿轴向方向发生金属流动,开缝芯棒第一次孔挤压强化孔壁材料的金属流动由试样孔壁挤入端流向孔壁挤出端,开缝芯棒第一次挤压强化后带孔试样翻转180°,开缝芯棒第一次挤压强化试样孔壁的挤入端是开缝芯棒第二次挤压强化试样的挤出端,开缝芯棒第一次挤压强化试样孔壁的挤出端是开缝芯棒第二次挤压强化试样孔壁的挤入端,开缝芯棒第二次孔挤压强化孔壁材料的金属流动由试样孔壁挤出端流向挤入端,开缝芯棒异向两次孔挤压强化后试样孔壁挤入端、挤出端塑性变形程度较均匀,孔壁挤入端、挤出端形成的残余压应力较均匀。
方案3“开缝芯棒同向两次挤压强化”、方案4“开缝芯棒异向两次挤压强化”,开缝芯棒对带孔试样进行了两次挤压强化,且开缝芯棒进行第二次孔挤压强化时将开缝芯棒旋转一定角度,消除了开缝芯棒第一次孔挤压强化时孔壁形成的凸脊,带孔试样经过两次挤压强化后孔壁材料的塑性变形程度大于开缝芯棒一次挤压强化,引起带孔试样两次挤压强化后试样孔壁形成的残余压应力大于开缝芯棒一次挤压强化。开缝芯棒进行第二次挤压强化时,开缝芯棒需要旋转10°~30°。由于开缝芯棒存在开缝,开缝芯棒孔挤压强化后试样孔壁形成凸脊,若开缝芯棒进行第二次孔挤压强化时与第一次孔挤压强化时开缝芯棒的位置、方向相同,开缝芯棒第二次挤压强化后孔壁形成的凸脊未消失,且凸脊高度大于第一次孔挤压强化后试样孔壁形成的凸脊高度。开缝芯棒第二次孔挤压强化时将开缝芯棒旋转10°~30°,开缝芯棒第二次孔挤压强化能够消除开缝芯棒第一次孔挤压强化后孔壁形成的凸脊。若开缝芯棒进行第二次孔挤压强化时开缝芯棒旋转的角度太小或太大,将无法消除开缝芯棒第一次孔挤压强化后孔壁形成的凸脊。
综上所述,方案4的孔挤压强化效果最佳,即将带孔试样第一次开缝芯棒孔挤压强化后,由于开缝芯棒存在开缝,开缝芯棒孔挤压强化后试样孔壁形成凸脊。然后将试样翻转180°,使开缝芯棒第一次孔挤压强化试样的挤入端作为开缝芯棒第二次孔挤压强化试样的挤出端,开缝芯棒第一次孔挤压强化试样的挤出端作为开缝芯棒第二次孔挤压强化试样的挤入端,且将开缝芯棒旋转10°~30°,进行开缝芯棒的第二次挤压强化,提升孔周残余应力均匀化程度。In summary,
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