Citation: | LIU Rujun, HUANG Xiang, HUANG Haihong, TAO Meisheng, YIN Chaochao, BAN Xukeling. Numerical Simulation and Experimental Study on Secondary Cold Extrusion Strengthening of Pressed Bush[J]. Mechanical Science and Technology for Aerospace Engineering, 2024, 43(7): 1142-1150. doi: 10.13433/j.cnki.1003-8728.20240071 |
[1] |
陈忱, 曹瑶琴, 宋颖刚, 等. 直升机旋翼关键零件孔挤压强化工艺应用研究[J]. 直升机技术, 2016(4): 38-42. doi: 10.3969/j.issn.1673-1220.2016.04.009
CHEN C, CAO Y Q, SONG Y G, et al. Application research about hole extrusion process of key component of helicopter rotor hub[J]. Helicopter Technique, 2016(4): 38-42. (in Chinese) doi: 10.3969/j.issn.1673-1220.2016.04.009
|
[2] |
万里, 邓运来, 范世通. 时效处理对7050铝合金厚板材料组织、性能及残余应力的影响[J]. 中国有色金属学报, 2018, 28(7): 1277-1283. https://www.cnki.com.cn/Article/CJFDTOTAL-ZYXZ201807001.htm
WAN L, DENG Y L, FAN S T. Effects of aging on microstructures, properties and residual stress of 7050 aluminum alloy[J]. The Chinese Journal of Nonferrous Metals, 2018, 28(7): 1277-1283. (in Chinese) https://www.cnki.com.cn/Article/CJFDTOTAL-ZYXZ201807001.htm
|
[3] |
KIM H K, CARLSON S S, STANFIELD M L, et al. Mitigating cutting-induced plasticity errors in the determination of residual stress at cold expanded holes using the contour method[J]. Experimental Mechanics, 2022, 62(1): 3-18. doi: 10.1007/s11340-021-00756-z
|
[4] |
KUMAR S A, BABU N C M. Effect of proximity hole on induced residual stresses during cold expansion of adjacent holes[J]. Materials Today: Proceedings, 2018, 5(2): 5709-5715. doi: 10.1016/j.matpr.2017.12.165
|
[5] |
张铁亮, 王卓, 宋镝冲, 等. 紧固件防松性能定量评价方法[J]. 机械工程学报, 2021, 57(15): 71-79. https://www.cnki.com.cn/Article/CJFDTOTAL-JXXB202115008.htm
ZHANG T L, WANG Z, SONG D C, et al. Quantitative evaluation method of anti-loosening performance for fasteners[J]. Journal of Mechanical Engineering, 2021, 57(15): 71-79. (in Chinese) https://www.cnki.com.cn/Article/CJFDTOTAL-JXXB202115008.htm
|
[6] |
WARNER J J, CLARK P N, HOEPPNER D W. Cold expansion effects on cracked fastener holes under constant amplitude and spectrum loading in the 2024-T351 aluminum alloy[J]. International Journal of Fatigue, 2014, 68: 209-216. doi: 10.1016/j.ijfatigue.2014.05.002
|
[7] |
WEN S Z, LIU C Y, WU R L, et al. Effect of cold expansion on high cycle fatigue of 7A85 aluminum alloy straight lugs[J]. Rare Metal Materials and Engineering, 2015, 44(10): 2358-2362. doi: 10.1016/S1875-5372(16)30020-0
|
[8] |
WANG Y L, ZHU Y L, HOU S, et al. Investigation on fatigue performance of cold expansion holes of 6061-T6 aluminum alloy[J]. International Journal of Fatigue, 2017, 95: 216-228. doi: 10.1016/j.ijfatigue.2016.10.030
|
[9] |
王燕礼, 卞小芳, 符彬, 等. 光整滚光和开缝衬套挤压孔结构表面完整性及疲劳行为研究[J]. 表面技术, 2019, 48(9): 336-345. https://www.cnki.com.cn/Article/CJFDTOTAL-BMJS201909042.htm
WANG Y L, BIAN X F, FU B, et al. Surface integrity and fatigue behaviour of holes treated by finishing & burnishing and split sleeve cold expansion[J]. Surface Technology, 2019, 48(9): 336-345. (in Chinese) https://www.cnki.com.cn/Article/CJFDTOTAL-BMJS201909042.htm
|
[10] |
王燕礼, 朱有利, 曹强, 等. 孔挤压强化技术研究进展与展望[J]. 航空学报, 2018, 39(2): 021336. https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201802001.htm
WANG Y L, ZHU Y L, CAO Q, et al. Progress and prospect of research on hole cold expansion technique[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(2): 021336. (in Chinese) https://www.cnki.com.cn/Article/CJFDTOTAL-HKXB201802001.htm
|
[11] |
张志贤, 张立新, 王凡. 压合衬套强化耳片的疲劳寿命评估[J]. 航空科学技术, 2022, 33(3): 97-105. https://www.cnki.com.cn/Article/CJFDTOTAL-HKKX202203013.htm
ZHANG Z X, ZHANG L X, WANG F. Evaluation of fatigue life of lug with cold expanded bushing[J]. Aeronautical Science & Technology, 2022, 33(3): 97-105. (in Chinese) https://www.cnki.com.cn/Article/CJFDTOTAL-HKKX202203013.htm
|
[12] |
唐伟, 林忠亮, 吴保全, 等. 孔结构压合衬套冷挤压强化的疲劳寿命试验研究[J]. 航空精密制造技术, 2022, 58(4): 11-15. https://www.cnki.com.cn/Article/CJFDTOTAL-HJZJ202204003.htm
TANG W, LIN Z L, WU B Q, et al. Test study on fatigue life of cold extrusion strengthening bushings for hole structure[J]. Aviation Precision Manufacturing Technology, 2022, 58(4): 11-15. (in Chinese) https://www.cnki.com.cn/Article/CJFDTOTAL-HJZJ202204003.htm
|
[13] |
杨广勇, 李萌, 宋颖刚, 等. 二次孔挤压强化对Ti1023钛合金孔疲劳性能影响[J]. 航空材料学报, 2016, 36(6): 68-73. https://www.cnki.com.cn/Article/CJFDTOTAL-HKCB201606012.htm
YANG G Y, LI M, SONG Y G, et al. Effect of twice hole expansion on fatigue property of Ti1023 alloy[J]. Journal of Aeronautical Materials, 2016, 36(6): 68-73. (in Chinese) https://www.cnki.com.cn/Article/CJFDTOTAL-HKCB201606012.htm
|
[14] |
姜廷宇, 王洋, 王鹏, 等. TB6钛合金孔二次挤压残余应力及疲劳寿命仿真研究[J]. 航空制造技术, 2021, 64(9): 77-84. https://www.cnki.com.cn/Article/CJFDTOTAL-HKGJ202109010.htm
JIANG T Y, WANG Y, WANG P, et al. Simulation study on residual stress and fatigue life of TB6 titanium alloy hole after double cold expansion[J]. Aeronautical Manufacturing Technology, 2021, 64(9): 77-84. (in Chinese) https://www.cnki.com.cn/Article/CJFDTOTAL-HKGJ202109010.htm
|
[15] |
罗学昆, 艾莹珺, 王欣, 等. 二次孔挤压强化对TB6钛合金疲劳性能的影响[J]. 航空材料学报, 2017, 37(6): 88-94. https://www.cnki.com.cn/Article/CJFDTOTAL-HKCB201706015.htm
LUO X K, AI Y J, WANG X, et al. Effect of double cold expansion of hole on fatigue property of TB6 titanium alloy[J]. Journal of Aeronautical Materials, 2017, 37(6): 88-94. (in Chinese) https://www.cnki.com.cn/Article/CJFDTOTAL-HKCB201706015.htm
|
[16] |
Battelle Memorial Institute. Metallic materials properties development and standardization (MMPDS-09)[M]. America: Federal Aviation Administration, 2014.
|
[17] |
王强, 赵勇, 倪孟龙. 高干涉量压合衬套强化铝合金孔结构的疲劳性能[J]. 机械工程材料, 2020, 44(7): 46-50. https://www.cnki.com.cn/Article/CJFDTOTAL-GXGC202007011.htm
WANG Q, ZHAO Y, NI M L. Fatigue properties of aluminum alloy hole structure strengthened by high interference fit bushing technique[J]. Materials for Mechanical Engineering, 2020, 44(7): 46-50. (in Chinese) https://www.cnki.com.cn/Article/CJFDTOTAL-GXGC202007011.htm
|
[18] |
ACHARD V, DAIDIE A, PAREDES M, et al. Optimization of the cold expansion process for titanium holes[J]. Advanced Engineering Materials, 2017, 19(6): 1500626.
|
[19] |
于洋, 罗学昆, 刘勇军, 等. 孔挤压强化对FGH95合金室温及高温疲劳性能的影响[J]. 航空制造技术, 2019, 62(18): 76-82. https://www.cnki.com.cn/Article/CJFDTOTAL-HKGJ201918021.htm
YU Y, LUO X K, LIU Y J, et al. Effect of hole cold expansion on fatigue property of FGH95 superalloy under room and high temperature[J]. Aeronautical Manufactur-ing Technology, 2019, 62(18): 76-82. (in Chinese) https://www.cnki.com.cn/Article/CJFDTOTAL-HKGJ201918021.htm
|
[20] |
BORREGO L P, COSTA J M, SILVA S, et al. Microstructure dependent fatigue crack growth in aged hardened aluminium alloys[J]. International Journal of Fatigue, 2004, 26(12): 1321-1331.
|