Improvement of fatigue strength of the plate with a hole

被引:0
|
作者
Nishida, S [1 ]
Wang, S [1 ]
Hattori, N [1 ]
Nakamura, N [1 ]
机构
[1] Saga Univ, Fac Sci & Engn, Saga 8408502, Japan
来源
SURFACE TREATMENT IV: COMPUTER METHODS AND EXPERIMENTAL MEASUREMENTS | 1999年 / 3卷
关键词
D O I
暂无
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
In this paper plane bending fatigue tests have been performed to investigate the effect of die-pressing on fatigue strength of specimens with a central circular hole notch. The main results obtained in this study are as follows: (1) By applying a die-press chamfering method, the fatigue limit of notched specimen increases with 63% higher than that of specimen without chamfering; The increment obtained by the above method is over 4 times of the increment obtained by the machining chamfering method. (2) The fatigue strength enhancing may attribute to the work-hardening and compressive residual stress that suppress the fatigue crack initiation and early stage propagation. (3) Though non-propagating micro-crack is not observed on the specimen without die-pressing chamfering the existence of the non-propagating micro-cracks in the specimen with die-press chamfering are observed.
引用
收藏
页码:361 / 370
页数:10
相关论文
共 50 条
  • [31] Investigation on residual strength of airplane plate with smooth circular hole
    Yao Wuwen
    Zhou Ping
    Hou Shengli
    Gao Yunkui
    2013 INTERNATIONAL CONFERENCE ON PROCESS EQUIPMENT, MECHATRONICS ENGINEERING AND MATERIAL SCIENCE, 2013, 331 : 31 - +
  • [32] Open-hole tension strength of pultruded GRP plate
    Turvey, GJ
    Wang, P
    PROCEEDINGS OF THE INSTITUTION OF CIVIL ENGINEERS-STRUCTURES AND BUILDINGS, 2003, 156 (01) : 93 - 101
  • [33] Improvement of traction-traction fatigue properties of A100 steel plate-hole-structure by double shot peening
    Zhi, Yinglin
    Zhang, Xiaohua
    Liu, Daoxin
    Yang, Jing
    Liu, Dan
    Guan, Yanying
    Shi, Jianmeng
    Zhao, Weidong
    Zhao, Ruiming
    Wu, Junnan
    Wang, Junbin
    Cheng, Shumin
    INTERNATIONAL JOURNAL OF FATIGUE, 2022, 162
  • [34] Improvement of traction-traction fatigue properties of A100 steel plate-hole-structure by double shot peening
    Zhi, Yinglin
    Zhang, Xiaohua
    Liu, Daoxin
    Yang, Jing
    Liu, Dan
    Guan, Yanying
    Shi, Jianmeng
    Zhao, Weidong
    Zhao, Ruiming
    Wu, Junnan
    Wang, Junbin
    Cheng, Shumin
    International Journal of Fatigue, 2022, 162
  • [35] Fatigue strength improvement of lap joints of thin steel plate using low-transformation-temperature welding wire
    Ohta, A.
    Matsuoka, K.
    Nguyen, N.T.
    Maeda, Y.
    Suzuki, N.
    Welding Journal (Miami, Fla), 2003, 82 (04):
  • [36] Fatigue strength improvement of lap joints of thin steel plate using low-transformation-temperature welding wire
    Ohta, A
    Matsuoka, K
    Nguyen, NT
    Maeda, Y
    Suzuki, N
    WELDING JOURNAL, 2003, 82 (04) : 78S - 83S
  • [37] Fatigue Strength around Through Hole in Printed Circuit Board
    Kinoshita, Takahiro
    Iwade, Shogo
    Shima, Shunpei
    Kawakami, Takashi
    Mizushina, Hideki
    Iinaga, Hiroshi
    2013 8TH INTERNATIONAL MICROSYSTEMS, PACKAGING, ASSEMBLY AND CIRCUITS TECHNOLOGY CONFERENCE (IMPACT), 2013, : 238 - 240
  • [38] A coupled strength and toughness criterion for the prediction of the open hole tensile strength of a composite plate
    Martin, E.
    Leguillon, D.
    Carrere, N.
    INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2012, 49 (26) : 3915 - 3922
  • [39] Fatigue strength improvement for ship structures by Ultrasonic Peening
    Deguchi, Takanori
    Mouri, Masashi
    Hara, Junya
    Kano, Daichi
    Shimoda, Taichiro
    Inamura, Fumihide
    Fukuoka, Tetsuji
    Koshio, Keisuke
    JOURNAL OF MARINE SCIENCE AND TECHNOLOGY, 2012, 17 (03) : 360 - 369
  • [40] Fatigue strength improvement for ship structures by Ultrasonic Peening
    Takanori Deguchi
    Masashi Mouri
    Junya Hara
    Daichi Kano
    Taichiro Shimoda
    Fumihide Inamura
    Tetsuji Fukuoka
    Keisuke Koshio
    Journal of Marine Science and Technology, 2012, 17 : 360 - 369