CN110408756A - Rotary Hole Cold Extrusion Strengthening Device and Method - Google Patents
Rotary Hole Cold Extrusion Strengthening Device and Method Download PDFInfo
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Abstract
本发明公开了一种旋转式孔冷挤压强化装置与方法,用于解决现有冷挤压装置导致孔周残余应力范围沿厚度方向分布不均的技术问题。技术方案是所述装置包括芯棒,还包括梯形挤压块、挤压驱动台、驱动手柄和制动挡块。所述方法中芯棒采用周向旋转运动代替轴向运动完成强化过程。即一端带有螺纹的芯棒在驱动手柄的配合下沿轴向运动推动梯形挤压块完成孔壁的局部挤压,利用制动挡块将芯棒与挤压驱动台、驱动手柄固连,旋转驱动手柄一周将梯形挤压块的挤压量均匀施加到孔周。采用旋转挤压强化的方式解决了残余应力在孔壁厚度方向不均的技术问题,使得在芯棒的入口处仍能获得较高的残余应力值,提升了孔周整体的疲劳强化效果。
The invention discloses a rotary hole cold extrusion strengthening device and method, which are used to solve the technical problem that the existing cold extrusion device causes the uneven distribution of the residual stress range around the hole along the thickness direction. The technical solution is that the device includes a mandrel, and also includes a trapezoidal extruding block, an extruding driving table, a driving handle and a braking block. In the method, the mandrel uses circumferential rotation instead of axial movement to complete the strengthening process. That is, the threaded mandrel at one end moves axially with the cooperation of the driving handle to push the trapezoidal extrusion block to complete the partial extrusion of the hole wall, and the mandrel is fixedly connected with the extrusion drive table and the driving handle by using the brake stopper. Rotate the driving handle for one circle to evenly apply the extrusion amount of the trapezoidal extrusion block to the circumference of the hole. The method of rotary extrusion strengthening solves the technical problem of uneven residual stress in the thickness direction of the hole wall, so that a higher residual stress value can still be obtained at the entrance of the mandrel, which improves the overall fatigue strengthening effect around the hole.
Description
技术领域technical field
本发明涉及一种旋转式孔冷挤压强化装置,还涉及一种旋转式孔冷挤压强化方法。The invention relates to a rotary hole cold extrusion strengthening device, and also relates to a rotary hole cold extrusion strengthening method.
背景技术Background technique
在航空制造领域,孔的冷挤压强化工艺能够很好地解决,机械连接孔受疲劳外载影响下孔周疲劳裂纹萌生的问题。其工艺方式是将一根经表面润滑、直径较大、硬度较高的圆锥形芯棒强行通过孔,这一过程迫使孔壁发生一系列的弹塑性变形,在孔周引入残余应力的同时消除了制孔机械损伤,从根本上减少了孔结构疲劳破坏的发生。In the field of aviation manufacturing, the cold extrusion strengthening process of the hole can well solve the problem of fatigue crack initiation around the hole under the influence of fatigue external load in the mechanical connection hole. The process method is to force a conical mandrel with lubricated surface, large diameter and high hardness through the hole. This process forces the hole wall to undergo a series of elastic-plastic deformation, and eliminates the residual stress while introducing residual stress around the hole. The mechanical damage of hole making is eliminated, and the occurrence of fatigue damage of hole structure is fundamentally reduced.
参照图4。文献“孔挤压强化技术研究进展与展望.航空学报.39-(2018):1-17.”公开了一种冷挤压装置。该装置包括芯棒3、开缝衬套8、顶帽9和拉枪10。在强化过程中首先将开缝衬套8安装在芯棒3的小直径端,然后将芯棒3和顶帽9分别从待强化孔2的两端安装到位,启动拉枪10将芯棒3从待强化孔2中拉出,完成连接孔的强化工艺。强化过程中由于孔最终要被胀大,孔壁材料承受巨大的挤压力在与挤压装置发生相对位移的过程中转化为摩擦力,导致孔壁材料随芯棒产生塑性流动。最终的结果使得孔壁材料逐渐向芯棒3挤出端聚集,造成挤出端的实际挤压量要大于挤入端的挤压量。强化工艺完成后残余应力范围沿孔壁厚度方向会呈梯形分布,孔挤出面最大,挤入面最小。挤入面较小的残余应力对于疲劳强化效果的贡献是有限的,此区域成为孔周材料抵抗疲劳破坏的薄弱环节。因此想进一步提高孔的冷挤压强化效果,残余应力沿孔壁厚度方向分布不均的问题必须得到妥善解决。Refer to Figure 4. The document "Research Progress and Prospects of Hole Extrusion Strengthening Technology. Acta Aeronautics Sinica. 39-(2018): 1-17." discloses a cold extrusion device. The device includes a mandrel 3 , a slotted bush 8 , a top cap 9 and a pulling gun 10 . In the strengthening process, the slotted bushing 8 is first installed on the small diameter end of the mandrel 3, and then the mandrel 3 and the top cap 9 are respectively installed in place from the two ends of the hole 2 to be strengthened, and the pulling gun 10 is started to pull the mandrel 3 into place. Pull out from the hole to be strengthened 2 to complete the strengthening process of the connecting hole. During the strengthening process, because the hole will eventually be expanded, the hole wall material bears a huge extrusion force and is converted into friction force during the relative displacement with the extrusion device, resulting in plastic flow of the hole wall material with the mandrel. The final result is that the material of the hole wall gradually gathers toward the extrusion end of the mandrel 3, causing the actual extrusion amount at the extrusion end to be greater than that at the extrusion end. After the strengthening process is completed, the residual stress range will be distributed in a trapezoid along the thickness direction of the hole wall, the extrusion surface of the hole is the largest, and the extrusion surface is the smallest. The contribution of the small residual stress on the extrusion surface to the fatigue strengthening effect is limited, and this area becomes the weak link of the material around the hole to resist fatigue damage. Therefore, in order to further improve the cold extrusion strengthening effect of the hole, the problem of uneven distribution of residual stress along the thickness direction of the hole wall must be properly resolved.
发明内容Contents of the invention
为了克服现有冷挤压装置导致孔周残余应力范围沿厚度方向分布不均的不足,本发明提供一种旋转式孔冷挤压强化装置与方法。所述装置包括芯棒,还包括梯形挤压块、挤压驱动台、驱动手柄和制动挡块。所述方法中芯棒采用周向旋转运动代替轴向运动完成强化过程。即一端带有螺纹的芯棒在驱动手柄的配合下沿轴向运动推动梯形挤压块完成孔壁的局部挤压,利用制动挡块将芯棒与挤压驱动台、驱动手柄固连,旋转驱动手柄一周将梯形挤压块的挤压量均匀施加到孔周。采用旋转挤压强化的方式解决了残余应力在孔壁厚度方向不均的技术问题,使得在芯棒的入口处仍能获得较高的残余应力值,提升了孔周整体的疲劳强化效果。In order to overcome the disadvantage of the existing cold extrusion device that the residual stress range around the hole is unevenly distributed along the thickness direction, the present invention provides a rotary hole cold extrusion strengthening device and method. The device includes a mandrel, and also includes a trapezoidal extruding block, an extruding driving table, a driving handle and a braking block. In the method, the mandrel uses circumferential rotation instead of axial movement to complete the strengthening process. That is, the threaded mandrel at one end moves axially under the cooperation of the driving handle to push the trapezoidal extrusion block to complete the partial extrusion of the hole wall, and the mandrel is fixedly connected with the extrusion drive table and the driving handle by using the brake stopper. Rotate the driving handle for one circle to evenly apply the extrusion amount of the trapezoidal extrusion block to the circumference of the hole. The method of rotary extrusion strengthening solves the technical problem of uneven residual stress in the thickness direction of the hole wall, so that a higher residual stress value can still be obtained at the entrance of the mandrel, which improves the overall fatigue strengthening effect around the hole.
本发明解决其技术问题所采用的技术方案是:一种旋转式孔冷挤压强化装置,包括芯棒3,其特点是:还包括梯形挤压块4、挤压驱动台5、驱动手柄6和制动挡块7。所述芯棒3一端为锥形斜面另一端带有螺纹,芯棒3的螺纹端与挤压驱动台5、驱动手柄6中心的螺纹孔配合。挤压驱动台5为带有筋条的圆柱凸台,底部圆台外侧留有突出部分,与驱动手柄6凹槽紧密配合传导扭矩。挤压驱动台5顶部凹槽内安放梯形挤压块4与芯棒3锥形斜面相配合。芯棒3螺纹端开有矩形通槽,驱动手柄6底部开有方槽,矩形通槽和方槽用于放入制动挡块7,限制芯棒3相对于驱动手柄6的周向转动,芯棒3圆锥形斜面为梯形挤压块4提供稳定支撑。The technical solution adopted by the present invention to solve the technical problem is: a rotary hole cold extrusion strengthening device, including a mandrel 3, which is characterized in that it also includes a trapezoidal extrusion block 4, an extrusion driving table 5, and a driving handle 6 and brake stop 7. One end of the mandrel 3 is a tapered inclined surface and the other end is threaded, and the threaded end of the mandrel 3 is matched with the threaded hole at the center of the extrusion drive table 5 and the drive handle 6 . The extruding drive table 5 is a cylindrical boss with ribs, and there is a protruding part on the outside of the bottom round table, which is closely matched with the groove of the driving handle 6 to transmit torque. A trapezoidal extrusion block 4 is placed in the top groove of the extruding drive table 5 to match the conical slope of the mandrel 3 . The threaded end of the mandrel 3 is provided with a rectangular through slot, and the bottom of the driving handle 6 is provided with a square slot. The rectangular through slot and the square slot are used to put the brake stopper 7 to limit the circumferential rotation of the mandrel 3 relative to the driving handle 6. The conical inclined surface of mandrel 3 provides stable support for trapezoidal extrusion block 4 .
一种旋转式孔冷挤压强化方法,其特点是包括以下步骤:A rotary hole cold extrusion strengthening method is characterized in that it includes the following steps:
步骤一、将装配体1顶部放置在待强化孔2内,芯棒3螺纹段与挤压驱动台5、驱动手柄6底部的螺纹孔相连接;Step 1. Place the top of the assembly 1 in the hole 2 to be strengthened, and connect the threaded section of the mandrel 3 with the threaded holes at the bottom of the extrusion drive table 5 and the drive handle 6;
步骤二、旋转驱动手柄6,芯棒3螺纹段进入驱动手柄6螺纹孔内,带动芯棒3圆锥形面对梯形挤压块4斜面施加压力,使梯形挤压块4沿径向外扩展,完成对待强化孔2局部孔壁的挤压;Step 2: Rotate the driving handle 6, the threaded section of the mandrel 3 enters the threaded hole of the driving handle 6, and drives the conical surface of the mandrel 3 to exert pressure on the inclined surface of the trapezoidal extrusion block 4, so that the trapezoidal extrusion block 4 expands radially outward, Complete the extrusion of the local hole wall of the hole 2 to be strengthened;
步骤三、局部孔壁挤压完成后,在芯棒3螺纹段通槽与驱动手柄6底部方槽中塞入制动挡块7,限制挤压芯棒相对于挤压驱动台5和驱动手柄6的周向旋转自由度。Step 3: After the extrusion of the local hole wall is completed, insert the brake block 7 into the through groove of the mandrel 3 threaded section and the square groove at the bottom of the drive handle 6 to limit the extrusion of the mandrel relative to the extrusion drive table 5 and the drive handle 6 degrees of circumferential rotational freedom.
步骤四、再次旋转驱动手柄6,使梯形挤压块4在待强化孔2孔壁内旋转一周,完成整个旋转冷挤压强化过程。Step 4: Rotate the driving handle 6 again, so that the trapezoidal extrusion block 4 rotates once in the wall of the hole 2 to be strengthened, and completes the entire rotary cold extrusion strengthening process.
本发明的有益效果是:所述装置包括芯棒,还包括梯形挤压块、挤压驱动台、驱动手柄和制动挡块。所述方法中芯棒采用周向旋转运动代替轴向运动完成强化过程。即一端带有螺纹的芯棒在驱动手柄的配合下沿轴向运动推动梯形挤压块完成孔壁的局部挤压,利用制动挡块将芯棒与挤压驱动台、驱动手柄固连,旋转驱动手柄一周将梯形挤压块的挤压量均匀施加到孔周。采用旋转挤压强化的方式解决了残余应力在孔壁厚度方向不均的技术问题,使得在芯棒的入口处仍能获得较高的残余应力值,提升了孔周整体的疲劳强化效果。The beneficial effect of the present invention is that: the device includes a mandrel, and also includes a trapezoidal extruding block, an extruding driving platform, a driving handle and a braking block. In the method, the mandrel uses circumferential rotation instead of axial movement to complete the strengthening process. That is, the threaded mandrel at one end moves axially under the cooperation of the driving handle to push the trapezoidal extrusion block to complete the partial extrusion of the hole wall, and the mandrel is fixedly connected with the extrusion drive table and the driving handle by using the brake stopper. Rotate the driving handle for one circle to evenly apply the extrusion amount of the trapezoidal extrusion block to the circumference of the hole. The method of rotary extrusion strengthening solves the technical problem of uneven residual stress in the thickness direction of the hole wall, so that a higher residual stress value can still be obtained at the entrance of the mandrel, which improves the overall fatigue strengthening effect around the hole.
以下结合附图和实施例详细说明本发明。The present invention will be described in detail below in conjunction with the accompanying drawings and embodiments.
附图说明Description of drawings
图1是本发明旋转式孔冷挤压强化装置的装配图。Fig. 1 is an assembly diagram of the rotary hole cold extrusion strengthening device of the present invention.
图2是本发明旋转式孔冷挤压强化装置的爆炸图。Fig. 2 is an exploded view of the rotary hole cold extrusion strengthening device of the present invention.
图3是图2中的梯形挤压块在孔壁施加局部挤压量的原理图。Fig. 3 is a principle diagram of the trapezoidal extruding block in Fig. 2 exerting a local extrusion amount on the hole wall.
图4是背景技术孔冷挤压装置的装配图。Fig. 4 is an assembly diagram of a hole cold extrusion device in the background technology.
图中,1-装配体,2-待强化孔,3-芯棒,4-梯形挤压块,5-挤压驱动台,6-驱动手柄,7-制动挡块,8-开缝衬套,9-顶帽,10-拉枪。In the figure, 1-assembly, 2-hole to be strengthened, 3-mandrel, 4-trapezoidal extrusion block, 5-extrusion drive table, 6-drive handle, 7-brake block, 8-slit liner Set, 9-top hat, 10-pull gun.
具体实施方式Detailed ways
参照图1-3。本发明旋转式孔冷挤压强化装置,包括芯棒3,还包括梯形挤压块4、挤压驱动台5、驱动手柄6和制动挡块7。芯棒3一端为锥形斜面另一端带有螺纹,芯棒3的螺纹端与挤压驱动台5、驱动手柄6中心的螺纹孔配合。挤压驱动台5为带有筋条的圆柱凸台,底部圆台外侧留有突出部分,与驱动手柄6凹槽紧密配合传导扭矩。挤压驱动台5顶部凹槽内安放梯形挤压块4与芯棒3锥形斜面相配合。在对孔局部孔壁挤压阶段,梯形挤压块4周向各面被挤压驱动台5圆柱上的方形槽孔限制。当芯棒3受力沿轴向运动时,由于梯形挤压块4周向各面被约束,芯棒3斜面上的反作用力只能推动梯形挤压块4向右侧移动,完成孔壁局部挤压量的施加。芯棒3螺纹端开有矩形通槽,当局部挤压完成后在驱动手柄6底部方槽与芯棒3通槽中塞入制动挡块7,限制芯棒3相对于驱动手柄6的周向转动,芯棒3圆锥形斜面为梯形挤压块4提供稳定支撑,保证局部挤压量在驱动手柄6旋转一周过程中施加到整个孔壁范围。Refer to Figure 1-3. The rotary hole cold extrusion strengthening device of the present invention includes a mandrel 3 , and also includes a trapezoidal extrusion block 4 , an extrusion drive table 5 , a drive handle 6 and a brake block 7 . One end of the mandrel 3 is a tapered inclined surface and the other end has threads, and the threaded end of the mandrel 3 cooperates with the threaded hole at the center of the extrusion drive table 5 and the drive handle 6 . The extruding drive table 5 is a cylindrical boss with ribs, and there is a protruding part on the outside of the bottom round table, which is closely matched with the groove of the driving handle 6 to transmit torque. A trapezoidal extrusion block 4 is placed in the groove on the top of the extruding drive table 5 to match the conical slope of the mandrel 3 . In the stage of extruding the partial hole wall of the hole, each circumferential surface of the trapezoidal extruding block 4 is limited by the square slots on the cylinder of the extruding driving platform 5 . When the mandrel 3 is forced to move in the axial direction, since the trapezoidal extrusion block 4 is constrained on all sides, the reaction force on the inclined surface of the mandrel 3 can only push the trapezoidal extrusion block 4 to move to the right to complete the hole wall part. The amount of squeeze applied. The threaded end of the mandrel 3 is provided with a rectangular through groove, and when the local extrusion is completed, a brake block 7 is inserted into the square groove at the bottom of the driving handle 6 and the through groove of the mandrel 3 to limit the circumference of the mandrel 3 relative to the driving handle 6. To rotate, the conical inclined surface of the mandrel 3 provides stable support for the trapezoidal extrusion block 4, ensuring that the local extrusion amount is applied to the entire range of the hole wall when the driving handle 6 rotates one circle.
一种旋转式孔冷挤压强化方法具体包括以下步骤:A rotary hole cold extrusion strengthening method specifically includes the following steps:
步骤一、将装配体1顶部放置在待强化孔2内,芯棒3螺纹段与挤压驱动台5、驱动手柄6底部的螺纹孔相连接;Step 1. Place the top of the assembly 1 in the hole 2 to be strengthened, and connect the threaded section of the mandrel 3 with the threaded holes at the bottom of the extrusion drive table 5 and the drive handle 6;
步骤二、旋转驱动手柄6,芯棒3螺纹段进入驱动手柄6螺纹孔内,带动芯棒3圆锥形面对梯形挤压块4斜面施加压力,使梯形挤压块4沿径向外扩展,完成对待强化孔2局部孔壁的挤压;Step 2: Rotate the driving handle 6, the threaded section of the mandrel 3 enters the threaded hole of the driving handle 6, and drives the conical surface of the mandrel 3 to exert pressure on the inclined surface of the trapezoidal extrusion block 4, so that the trapezoidal extrusion block 4 expands radially outward, Complete the extrusion of the local hole wall of the hole 2 to be strengthened;
步骤三、局部孔壁挤压完成后,在芯棒3螺纹段通槽与驱动手柄6底部方槽中塞入制动挡块7,限制挤压芯棒相对于挤压驱动台5和驱动手柄6的周向旋转自由度。Step 3: After the extrusion of the local hole wall is completed, insert the brake block 7 into the through groove of the mandrel 3 threaded section and the square groove at the bottom of the drive handle 6 to limit the extrusion of the mandrel relative to the extrusion drive table 5 and the drive handle 6 degrees of circumferential rotational freedom.
步骤四、再次旋转驱动手柄6,使梯形挤压块4在待强化孔2孔壁内旋转一周,完成整个旋转冷挤压强化过程。Step 4: Rotate the driving handle 6 again, so that the trapezoidal extrusion block 4 rotates once in the wall of the hole 2 to be strengthened, and completes the entire rotary cold extrusion strengthening process.
本发明通过将芯棒3抽拉式挤压改为旋转式挤压的方式,有效的避免了孔壁材料随芯棒3轴向流动所造成的孔壁出口处实际挤压量增大,残余应力大小沿厚度方向分布不均的技术问题。本发明强化方法引入的残余应力层更加均匀,提升了芯棒挤入面的残余应力大小,消除了强化效果的薄弱环节。In the present invention, by changing the pulling extrusion of mandrel 3 to rotary extrusion, it effectively avoids the increase of the actual extrusion amount at the outlet of the hole wall caused by the axial flow of the hole wall material with the mandrel 3, and the remaining The technical problem of uneven distribution of stress along the thickness direction. The residual stress layer introduced by the strengthening method of the present invention is more uniform, the residual stress of the mandrel extrusion surface is increased, and the weak link of the strengthening effect is eliminated.
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Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111022430A (en) * | 2019-12-25 | 2020-04-17 | 广东工业大学 | Bushing pipe structure, small hole strengthening device thereof and small hole fatigue strength improving method |
CN111118270A (en) * | 2019-12-31 | 2020-05-08 | 西北工业大学 | Cold extruding process and device for homogenizing residual stress around hole |
CN111635983A (en) * | 2020-06-12 | 2020-09-08 | 四川大学 | A tension-torsion coupling cold extrusion strengthening mandrel with holes and strengthening method thereof |
CN111635984A (en) * | 2020-06-12 | 2020-09-08 | 四川大学 | A hand-held tension-torsion coupling cold extrusion strengthening device and strengthening method for holes |
CN111975283A (en) * | 2020-07-24 | 2020-11-24 | 中国航发北京航空材料研究院 | Cold extrusion method and tooling for improving cycle life of wheel disc with bolt holes |
CN112680677A (en) * | 2020-12-09 | 2021-04-20 | 南京航空航天大学 | Process for reinforcing assembly hole by adopting slotted core rod cold extrusion |
CN112961967A (en) * | 2021-02-03 | 2021-06-15 | 四川大学 | Single-side cold extrusion fatigue strengthening device and method for orifice of open pore structure |
CN115652047A (en) * | 2022-10-08 | 2023-01-31 | 南京航空航天大学 | A slotted mandrel extrusion strengthening process to improve the uniformity of residual stress around the hole |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2005007314A1 (en) * | 2003-07-10 | 2005-01-27 | Fatigue Technology, Inc. | Fatigue enhancement of material surrounding openings in workpieces |
CN202164331U (en) * | 2011-06-08 | 2012-03-14 | 沈阳飞机工业(集团)有限公司 | Extruder |
CN203918350U (en) * | 2014-07-01 | 2014-11-05 | 无锡亿利大机械有限公司 | The efficient milled head of cylinder inner bore |
CN109280751A (en) * | 2018-09-05 | 2019-01-29 | 华东理工大学 | A kind of Hertz contact rotary extrusion strengthening device and strengthening process |
CN109304619A (en) * | 2018-09-21 | 2019-02-05 | 华东理工大学 | Variable diameter rotary cold extrusion strengthening process device |
-
2019
- 2019-07-15 CN CN201910637084.2A patent/CN110408756B/en active Active
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2005007314A1 (en) * | 2003-07-10 | 2005-01-27 | Fatigue Technology, Inc. | Fatigue enhancement of material surrounding openings in workpieces |
CN202164331U (en) * | 2011-06-08 | 2012-03-14 | 沈阳飞机工业(集团)有限公司 | Extruder |
CN203918350U (en) * | 2014-07-01 | 2014-11-05 | 无锡亿利大机械有限公司 | The efficient milled head of cylinder inner bore |
CN109280751A (en) * | 2018-09-05 | 2019-01-29 | 华东理工大学 | A kind of Hertz contact rotary extrusion strengthening device and strengthening process |
CN109304619A (en) * | 2018-09-21 | 2019-02-05 | 华东理工大学 | Variable diameter rotary cold extrusion strengthening process device |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN111022430A (en) * | 2019-12-25 | 2020-04-17 | 广东工业大学 | Bushing pipe structure, small hole strengthening device thereof and small hole fatigue strength improving method |
CN111118270A (en) * | 2019-12-31 | 2020-05-08 | 西北工业大学 | Cold extruding process and device for homogenizing residual stress around hole |
CN111118270B (en) * | 2019-12-31 | 2022-08-02 | 西北工业大学 | Cold extrusion process and device for homogenization of residual stress around holes |
CN111635983A (en) * | 2020-06-12 | 2020-09-08 | 四川大学 | A tension-torsion coupling cold extrusion strengthening mandrel with holes and strengthening method thereof |
CN111635984A (en) * | 2020-06-12 | 2020-09-08 | 四川大学 | A hand-held tension-torsion coupling cold extrusion strengthening device and strengthening method for holes |
CN111635983B (en) * | 2020-06-12 | 2021-02-26 | 四川大学 | A tension-torsion coupling cold extrusion strengthening mandrel with holes and strengthening method thereof |
CN111975283A (en) * | 2020-07-24 | 2020-11-24 | 中国航发北京航空材料研究院 | Cold extrusion method and tooling for improving cycle life of wheel disc with bolt holes |
CN111975283B (en) * | 2020-07-24 | 2023-03-14 | 中国航发北京航空材料研究院 | Cold extrusion method and tool for prolonging cycle life of wheel disc with bolt holes |
CN112680677A (en) * | 2020-12-09 | 2021-04-20 | 南京航空航天大学 | Process for reinforcing assembly hole by adopting slotted core rod cold extrusion |
CN112961967A (en) * | 2021-02-03 | 2021-06-15 | 四川大学 | Single-side cold extrusion fatigue strengthening device and method for orifice of open pore structure |
CN115652047A (en) * | 2022-10-08 | 2023-01-31 | 南京航空航天大学 | A slotted mandrel extrusion strengthening process to improve the uniformity of residual stress around the hole |
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