¤¤¤åºK­n¡G
¥»¬ã¨s¥D¦®¦b±´°Q¤£¦P¼ö³B²zª¬ºA¹ï17-4 PH»PCustom 450¤£ù׿û»G»k¯h³Ò©Ê½è¤§¼vÅT¡C¤ñ¸û¦b»G»kÀô¹Ò¤¤(3.5 wt% NaCl) ¤£¦P¼ö³B²zªº¯h³Ò¹Ø©R©M¯h³ÒµõÁ_¦¨ªøªº®t²§©Ê¡C¦b¯h³ÒµõÁ_¦¨ªø¹êÅç¤è­±¡A¦P®É°O¿ýµõÁ_³¬¦X®ÄÀ³¡A¥HÁA¸ÑµõÁ_³¬¦X®ÄÀ³¹ï¯h³ÒµõÁ_¦¨ªø³t²v¤§¼vÅT¡C¦¹¥~¡A¥ç§Q¥Î¥ú¾ÇÅã·LÃè(OM)©M±½´y¦¡¹q¤lÅã·LÃè(SEM)¡A¹ïª÷¬Û²Õ´»P¯}Â_­±¥[¥HÆ[¹î¤ÀªR¡A¥HÁA¸ÑµõÁ_ªº¥Í¦¨¤Î¦¨ªø¼Ò¦¡¡C¹êÅçµ²ªGÅã¥Ü¡A¨â´Ú¤£ù׿û¦b»G»kÀô¹Ò¤U¤§°ª¶g¯h³Ò©Ê½è¡A¨äH900³»®É®Ä³£¤ñH1150¹L®É®Ä³B²z¦³¸û°ª¤§»G»k¯h³Ò¹Ø©R¡A©T·»³B²z¤¶©ó¨âªÌ¤§¶¡¡C¦Ó¦b¯h³ÒµõÁ_¦¨ªø³t²v¤è­±¡A¨â´Ú¤£ù׿û¤§¹L®É®Ä³B²z¥Ñ©ó¦³¸û¨Î¤§¶´©Ê¤Î¸û¨Î­@²B¯Ü©è§Ü¤O¡A¨Ï¨ä¦³¤ñ³»®É®Ä¤Î©T·»³B²z¸û§C¤§¯h³ÒµõÁ_¦¨ªø³t²v¡CCustom 450¤£ù׿û¦b¦UºØ¹ïÀ³ªº¼ö³B²z±ø¥ó¤U³£¸û17-4 PH¤£ù׿û¦³¸û¨Î¤§¶´©Ê¡A¨Ï¨ä¦b¬Û¹ïÀ³¼ö³B²z¤U¨ã¦³¸û§Cªº¯h³ÒµõÁ_¦¨ªø³t²v¡C¥Ñ°ª¶g¯h³Ò©Ê½è¤Î¯h³ÒµõÁ_¦¨ªø³t²v¤§¤ñ¸ûÅã¥Ü¦¹¨â´Ú¤£ù׿û¦b»G»kÀô¹Ò¤¤¡A¥D¾É°ª¶g¯h³Ò¹Ø©Rªøµuªº­n¯À¬°µõÁ_°_©l¶¥¬q¡A¦Ó¤£¦bµõÁ_©µ¦ù¶¥¬q¡A¥Ñ©ó³»®É®Ä¤ñ¹L®É®Ä¤Î©T·»³B²z¦³¸û°ª­°¥ñ±j«×¤Î¸û¨Î¤§­@¤Õ»k©Ê½è¡A¦]¦Ó¦³¸û°ª¤§§ÜµõÁ_°_©lªý¤O¡A¾É­P¨ä¾ãÅé¯h³Ò¹Ø©R¸û°ª¡C¨â´Ú¤£ù׿û¦b¦P¤@¼ö³B²z±ø¥ó¤U¤§°ª¶g»G»k¯h³Ò¹Ø©R¤¬¬Û¤ñ¸û¥çÅã¥Ü¡A¨ã¦³¸û°ª­°¥ñ±j«×¤§§÷®Æ¦¨¤À»P¼ö³B²z²Õ¦X¡A¥ç¬Û¹ï¨ã¦³¸ûªøªº°ª¶g»G»k¯h³Ò¹Ø©R¡C¥ÑSEMÆ[¹î¤¤±oª¾¡A»G»k¯h³Òªº°_·½¬O¥Ñ»G»k²G«I»kªº»k¤Õ³B§Î¦¨¡A¨Ã¦³¦Ð¤òª¬ªe¬y¯¾¸ô¥Ñ°_©l³B¦V¥~ÂX´²©µ¦ù¡AµõÁ_©µ¦ù§e¬ï´¹¨«¦V¡A¦b©µ¦ù¤¤¯d¤U¯h³Ò¯¾¸ô¡A³Ì«á¯}Â_«h§e©µ©Ê¯}Ãa¼Ò¦¡¡C
Abstract¡G
This study investigated the corrosion fatigue properties of 17-4 PH and Custom 450 stainless steels in different heat treatments. In particular, the fatigue life and fatigue crack growth rate in 3.5 wt% NaCl solution for specimens in various tempers were compared. The effect of environmentally induced cracking mechanisms on the degradation of fatigue resistance was characterized. Fractography and microstructure analyses with scanning electron microscopy (SEM) and optical microscopy (OM) were conducted to determine the corrosion fatigue crack initiation and propagation mode. Results showed in both 17-4 PH and Custom 450 stainless steels the smooth specimens in H900 peak aged temper exhibited longer corrosion fatigue lives than the H1150 overaged ones while those in solution annealed temper lie between them. However, the overaged temper in these two stainless steels exhibited superior corrosion fatigue crack growth resistance to the other two tempers as a result of its greater toughness and lower susceptibility to hydrogen embrittlement. Custom 450 stainless steel in each temper had greater toughness than 17-4 PH one leading to a lower fatigue crack growth rate. Comparison of S-N and fatigue crack growth rate curves indicated that crack initiation stage played the major role in determining the entire corrosion fatigue life for both stainless steels in various tempers. The peak aged process which generated the highest yield strength exhibited the greater resistance to crack initiation and the longer corrosion fatigue life, as compared to the overaged and solution annealed conditions. In overall comparison, the greatest corrosion fatigue resistance of smooth specimen among these two stainless steels in various tempers is possessed by the temper with the highest yield strength. Fractography analyses indicated that corrosion fatigue cracks initiated mostly from corrosion pits followed by feathery river line features and striations as the cracks grew stably until final fracture. The corrosion fatigue cracks propagated in a transgranular mode for all tempers tested in this study.