camnetics
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camnetics
AISI 4340 Fatigue Life Assessment of Weld Surfacing of AISI 4340 9 :9; Siva Sitthipong :; ?@A B 9CDEDFF99DGEHID 9E E ; A Thesis Submitted in Partial Fulfillment of the Requirements for the Degree of Master of Engineering in Material Engineering Prince of Songkla University 2553 :WE ; ชื่อวิทยานิพนธ์ ผู้เขียน สาขาวิชา ปี การศึกษา การประเมินอายุความล้าของผิวเชื่อมพอกเหล็กกล้าทนแรงดึงสู ง AISI 4340 นายศิวะ สิ ทธิพงศ์ วิศวกรรมวัสดุ 2552 บทคัดย่ อ งานวิจยั นี้ เป็ นการวิเคราะห์การชารุ ดของเพลาสวิง ซึ่งผลิตมาจากเหล็กกล้า ผสมต่า ทนแรงดึงสู ง เกรด AISI 4340 ซึ่ งใช้ในระบบส่ งกาลังแบบหมุนเหวีย่ งของรถขุดไฟฟ้ า ประโยชน์ที่ ได้จากงานวิจยั นี้คือสามารถเลือกกรรมวิธีการเชื่อมซ่อมที่ดีที่สุดที่จะนามาใช้ในการเชื่อมซ่อมเพลา สวิงได้ หลังจากเพลาสวิงชารุ ดมีการตรวจพินิจผิวรอยแตกของเพลาสวิงพบว่ารอยแตกเริ่ มต้นจาก บริ เวณฟิ ลเลต เมื่อทาการศึกษาหาสาเหตุเพื่อแก้ปัญหา ผลจากการวิเคราะห์ค่าความเค้นสามารถ พิสูจน์และนาไปสู่ ทางออกของปั ญหาได้ โดยศึกษาในเงื่อนไขเพลาสวิงรับภาระเต็มกาลังขณะ ทางาน พบว่าบริ เวณที่มีค่าความเค้นสู งที่สุดเป็ นบริ เวณเดียวกันกับบริ เวณที่เพลาแตกขาด ความเค้น สู งสุ ดขณะที่เพลาเกิดการเปลี่ยนแปลงภาระกะทันหันถูกเชื่อว่าเป็ นสาเหตุเบื้องต้นของการแตกล้า และการลุกลามของรอยแตก จากการวิเคราะห์การชารุ ดยืนยันว่าสาเหตุมาจากการทางานที่ภาระไม่ ปกติ ท้ายที่สุดจะทาการแนะนากรรมวิธีการเชื่อมซ่อมที่เหมาะสมที่สุดในการซ่อมเพลาสวิง (3) Thesis Title Author Major Program Academic Year Fatigue Life Assessment of Weld Surfacing of AISI 4340 Mr. Siva Sitthipong Material Engineering 2009 ABSTRACT This research is to analyze the failure of swing shaft made of high strength steel AISI 4340 and use in the swing power transmission system of Electric Shovels. The advantage of this analysis is to select the best welding process to repair the shaft. After having fractured surface, visual examination of the fractured surface indicates cracks initiated from the fillet shoulder. To find out the cause of fracture of the shaft, the analytical solution was carried out to investigate the stress of the shaft under full loading during working. Result of stress analysis reveal that the maximum stress area was at the fractured regions of the damaged shaft. The maximum stresses predict under shock loading was believed to be the cause for fatique crack initiation and propagation of this failure. The failure analysis confirmed that the fatigue fracture of the shaft was caused by abnormal operation. Finally, some advices to select the best welding process are discussed of this swing shaft. 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(Stress Raiser) Á¡·É¤ ¹ÊĦ· Áª´¨nµª´ÂĦ¼ ¸É 1.9 Án¦°¥µ (Notch) ¤»¤nµ (Fillet) ¦¼ (Hole) ¦n ° (Groove) ¦°¥Â (Crack) ¹ÉÁ·µµ¦°°Â®¦º °¨µµ¦ Äo·ÊµÎµÄ®o¦· Áª´¨nµª°µ¤¸ªµ¤Áo¼Á·ªµ¤Â Ȧ¦µÂ¨³¦· Áªªµ¤ Á o¤ oªµ¤Áo³ÁÈ »Á¦·É ¤ °¦°¥ÂÁ¤°´ÂĦ¼ ¸É 1.10 ¦¼ ¸É 1.9 ¨´¬³¦· Áª¸É¤¸ªµ¤Á o¤ o °ªµ¤Áo¼ ¸É¤µ: Peterson (1974) ¦¼ ¸É 1.10 ¦· ÁªÁ¦·É ¤o °¦°¥Â ¸É¤µ: Xiaolei and Zhiwei (2008) c) »¤´ · °ª´» (Materials Properties) ¹ÉÂn¨³·³¤¸¤´·Å¤nÁ®¤º°´ ¤´· nµÇÁ¨¸É¥Â¨µ¤nª¤µÁ¤¸ (Chemical Composition) ´· °Ã¦¦oµ »¨£µ ¨³Á¨¸É¥Â¨µ¤¦³ªµ¦¨· Án¦³ªµ¦ ¹Ê¦¼ (Forming) ¨³ ¦³ªµ¦°»µªµ¤¦o°¤´ · °ª´»¸ÉÁ¨¸É¥Â¨ÅÅoÂn ªµ¤Â Ȧ¹ ªµ¤Â Ȧ¦µªµ¤Â Ȧ¦³Âªµ¤Â Ȫµ¤oµµµ¦¨oµ ´ÂĦ¼ ¸É1.11 ¦¼ ¸É 1.11 ¨ °Ã¦¦oµ»¨£µn° ¸Îµ´ªµ¤µ ¸É¤µ: ·· (2550) A= Á¢°¦rŦr B= Á¢°¦rŦr+Á¡°¦rŨr C= Á¡°¦rŨrD= °´Á¤Á°¦r¤µ¦rÁÅr E = Á¤Á°¦r¤µ¦rÁÅrF = Á¤Á°¦r¤µ¦rÁÅr + Á¤Á°¦rÁÅr G = Á¤Á°¦rÁÅr H= °°ÁÅr 1.2.3.2 ªµ¤Â Ȧ¨oµ (Fatigue Strength) ªµ¤Â Ȧ¨oµÅoµµ¦° °Wohler (1871) ´·ÊµÂµ®¤» £µ¥Äo¦¨´ (Alternative Force) Á¡ºÉ°µ¦®µªµ¤´¤¡´r¦³®ªnµªµ¤Áo´°µ¥» (¦°) ¨³ 媵¤Áo °·Êµ°¸ÉµÎ ¦» ´¦°¸ÉÅoÁ ¸¥¦µ¢ªµ¤Áo -¤µ¦µnª¨°µ¨·¹¤ ´¦°µ¦Îµ¦» Á¦¸ ¥ªnµS-N Curve ´ÂĦ¼ ¸É1.12 µS-N Curve °Ã¨®³¨»n¤Á®¨Èµ¤µ¦Ânnª°µ¥» °¦µ¢Åo 3 nªÄ Ân¨³nª¤¸ªµ¤´Å¤nÁnµ´º°nªÂ¦ÁÈ nª°µ¥»¦°Îɵ (Low Cycle) Fuch and Stepens (1980) ·¥µ¤Ä®oÁÈ nª¸É¤¸°µ¥» 0-1,000 ¦°Änª¸Ênµªµ¤  È¦¨oµ (fatique strength) ³ ¨¨°¥nµoµÇÁ¤ºÉ°Îµª¦°¸Éªµ¤Áo¦³ÎµÁ¡·É¤ ¹Ê¦³´É ¸É1,000¦°¡ªnµnµÂ Ȧ¨oµ (fatique strength) ¸É»¸Ê¤¸nµ 0.9 Sut ĵ·´ ·¦· oµ°µ¥»µ¦Äoµ °·Ênª°¥¼Än nª¸Ê ªnµ·Ênª´Ê®¤»oª¥ªµ¤Á¦È ª¦°¸ÉɵΠ¤µ¹°» è¤Åoªnµµ¦ª·´ ·¸ÉÁ· ¹Ê ÁÈ Â ·¥r(static) µ¤µ¦Äoµ¦ÎµªÂ·¥rÅo Änª¸É°Dieter (1986) ·¥µ¤Ä®oÁÈ nª°µ¥» 1,000-1,000,000 ¦°Änª¸Ê nµªµ¤Â Ȧ¨oµ (fatique strength) ³¨¨°¥nµ¦ªÁ¦È ªÁ¤ºÉ°Îµª¦°¸Éªµ¤Áo¦³Îµ¤¸nµ ¤µ ¹Êµ¦ª·´ ·Änª¸Ê³ÁÈ µ¦ª·´ ·Âµ¦¨oµ (fatique failure) oµÎµnµªµ¤Â Ȧ¨oµ (fatique strength) Änª¸ÊÅÄoĵ¦Îµª°°Â·Ênª¸ÉÅo³¤¸°µ¥»µ¦ÄoµÎµ´ (finite life) Änª¸É 3 º°nª°µ¥»¦°¼ (High Cycle) 媦°¸Éªµ¤Áo¦³ÎµÁ· 1,000,000 ¦°nµªµ¤Â Ȧ¨oµ (fatique strength) ¤¸nµ¸É°¥¼n ¸Énµ®¹É¹ÉÁ¦¸ ¥ªnµ endurance limit oµÎµnµ endurance limit ÅÄoĵ¦Îµª°°Â·Ênª¸ÉÅo³¤¸°µ¥»µ¦ÄoµÅ¤n ε´(infinite life) ¦¼ ¸É1.12 ´ª°¥nµ S-N Curves °Ã¨®³Ä¨»n¤Á®¨È ¸É¤µ: 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ª¦Îµshot peening ¦· Áª¢· ¨Á¨Â¨³¦ª°µ¦Â¦oµªµ¤Âµ¦ 妻 ¦´¬µ 85 บรรณานุกรม กฤษณพงษ เกียรติอนันต. การประเมินอายุความลาของโครงสรางสะพานสมเด็จพระพุทธยอดฟาชวง Bascule Span. วิทยานิพนธคณะวิศวกรรมศาสตร มหาวิทยาลัยธรรมศาสตร, 2546. จิตติ บัวพูน, นิรมิต เดชสุภา, ประศาสน สุบรรพวงศ และณรงคฤทธ โทธรัตน “การวิเคราะหการชํารุด เบื้ องต น ” สงขลา: ภาควิ ช าวิ ศ วกรรมเหมื องแร แ ละวัสดุ คณะวิศวกรรมศาสตร มหาวิทยาลัยสงขลานครินทร, 2550. ณรงค ฤ ทธ โทธรั ต น . อิ ท ธิ พ ลการให ค วามร อ นก อ นและหลั ง การเชื่ อ มบริ เ วณผลกระทบจาก ความร อนตอ อั ต ราการขยายตั ว ของรอยแตกจากความล าของเหล็ ก เกรดเอไอเอส ไอ 4340. กองโรงงานเหมืองแมเมาะ การไฟฟาฝายผลิตแหงประเทศไทย. การประชุม วิชาการ เครือขายวิศวกรรมเครื่องกลแหงประเทศไทยครั้งที่ 17 วันที่ 15-17 ตุลาคม 2546 จ. ปราจีนบุร.ี เดช พุ ท ธเจริ ญ ทอง. การวิ เ คราะห ด ว ยวิ ธี ไ ฟไนต เ อลิ เ มนต . ภาควิ ช าวิ ศ วกรรมเครื่ อ งกล คณะวิศวกรรมศาสตร มหาวิทยาลัยเทคโนโลยีพระจอมเกลาธนบุร,ี 2548. ธรรมนูญ สีดาคาร และ เกียรติฟา ตั้งใจจิต. “การศึกษารูปรางของบาเพลาที่มีผลตอความแข็งแรง ของเพลา 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And Preve.8 (2008): 75-80. 88 £µª 89 £µª ¦µ¥¨³Á°¸¥ °ÁºÊ°ª´»¸ÉÄoµÎ Á¡¨µª·Â¨³·ªÁºÉ°¤¡°Â¡¨µª· 90 Á®¨ÈAISI 4340 ´°¥¼Än ¨»n¤Á®¨È¨oµ¤Îɵ ¹É nµ¦³ªµ¦»Â Ȩ³° º´ªÎµÄ®o¤¸»¤´·µ¨¸ÉÁ®¤µ³¤´µ¨··Ên ªÁ¦ºÉ °¨Îµ®¦´µ®´¹É ¤¸ »¤´·nµÇ´¸Ê µ¦µ .1 Ân ª¤µÁ¤¸ °Á®¨ÈAISI 4340 C% 0.39 Mn% 0.74 Si% 0.19 P% 0.024 S% 0.019 Mo% 0.23 Ni% 1.72 Cr% 0.8 µ¦µ .2 »¤´·µ¨AISI 4340 ªµ¤Â Ȧ¹(MPa) ªµ¤Â Ȧ¦µ(MPa) °´¦µµ¦¥º´ª(%) µ¦¨ °£µ®oµ´(%) ªµ¤Â È(HV) 1044 918 16.2 42.9 320-340 ®¤µ¥Á®» Quenched & Tempered ¸É¤µ: Krupp Hoesch Stahlexpost GmbH Test Certificate No. 5/24496 Date: 05/1201995 Test required: AS PER DIN 50049-3.1B »¤´· °¨ªÁºÉ °¤ µ¦Á¨º°¨ªÁºÉ°¤Îµ®¦´ÁºÉ°¤Á®¨È AISI 4340 ¹ÉÁÈ Á®¨È¸É¤¸ªµ¤Â Ȧ¼ εÁÈ o° ¡·µ¦µªµ¤Â Ȧ¹ÁÈ ®¨´Â¨³ªµ¤¤µÁ¤¸°o °¥¼Än ¨»n¤Á¸¥ª´º°¨»n¤Á®¨È¨oµ¤ Îɵ ¨ªÁºÉ°¤®»¤o ¢¨´rÁ¨º°Äo¨ªÁºÉ°¤¤µ¦µ AWS A5.5-96 E11018- G H 4R (EN 757-1997 E696Mn2NiCrMoB42H5) Ã¥¤¸»¤´·´¸Ê 91 µ¦µ .3 Ân ª¤µÁ¤¸ °¨ªÁºÉ°¤®» ¤o ¢¨´r C% 0.05 Mn% 1.5 Si% 0.4 P% - S% - Mo% 0.5 Ni% 2.0 Cr% 0.4 µ¦µ .4 »¤´·µ¨ °¨ªÁºÉ°¤®»¤o ¢¨´r 840 ªµ¤Â Ȧ¹(MPa) 780 20 110 ¸É20 ȗC <5 ml/100g ªµ¤Â Ȧ¦µ(MPa) °´¦µµ¦¥º´ª(%) ªµ¤Â Ȧ¦³Â(Charpy-V) Joule ¦· ¤µµ¦Â¡¦n űæÁÄÁºÊ°ÁºÉ°¤ ¨ªÁºÉ°¤¤·/¤ Á¨º°Äo¨ªÁºÉ°¤µ¤¤µ¦µAWS A5.28-ER110S-G (EN 12534 Mn3NiCrMo) Ã¥¤¸»¤´·´¸Ê µ¦µ .5 Ân ª¤µÁ¤¸ °¨ªÁºÉ°¤¤·/¤ C% 0.1 Mn% 1.6 Si% 0.6 P% - S% - Mo% 0.25 µ¦µ .6 »¤´·µ¨ °¨ªÁºÉ°¤¤·/¤ ªµ¤Â Ȧ¹(MPa) ªµ¤Â Ȧ¦µ(MPa) °´¦µµ¦¥º´ª(%) ªµ¤Â Ȧ¦³Â(Charpy-V) Joule 900 800 19 190 ¸É20 ȗC Ni% 1.3 Cr% 0.25 92 ¨ªÁºÉ°¤Åo ¢¨´r Á¨º°Äo¨ªÁºÉ°¤¤µ¦µAWS A5.29-E110T-K4 (EN: 1999 12535 69 5 Mn2NiCrMo B3 H5) Ã¥¤¸»¤´·´¸Ê µ¦µ .7 Ân ª¤µÁ¤¸ °¨ªÁºÉ°¤Åo¢¨´r C% 0.05 Mn% 1.40 Si% 0.40 P% 0.005 S% 0.015 Mo% 0.50 µ¦µ¸É.8 »¤´·µ¨ °¨ªÁºÉ°¤Åo¢¨´r ªµ¤Â Ȧ¹(MPa) ªµ¤Â Ȧ¦µ(MPa) °´¦µµ¦¥º´ª(%) ªµ¤Â Ȧ¦³Â(Charpy-V) Joule 760 680 15 27 ¸É-51ȗC Ni% 2.40 Cr% 0.50 93 £µª µ¦®µ¦· ¤µµ¦r °Á¸¥Ánµ(Carbon Equivalence) 94 µ¦®µ¦· ¤µµ¦r °Á¸¥ÁnµÄÁ®¨È³ÁÈ ´¸°¹ªµ¤¥µnµ¥Äµ¦ÁºÉ°¤¹É µ¤µ¦®µÅoµ¤µ¦´¸Ê CE = C+ ( ݊ܯ+ܵ݅) 6 + ( ݎܥ+ܯ+ܸ) 5 + (ܰ݅+) ݑܥ 15 Ânµn ª¤µÁ¤¸µ£µª³ÅoCE = 0.87 µ¨µ¦ª·¥´ °Welding Technology Institute of Australia (1989) ÅoÂn¨»n¤Á®¨È °°ÁÈ 12 ¨»n¤µ¤¨µ¦Îµªnµ¦· ¤µµ¦r 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®¥»Á¦ºÉ °´¦Á¡ºÉ°°Á¨¸É¥°³Å®¨nn°¹¦° 妻 ¦´¬µ¹É ¤¸¨n°¦³µ¦¨·Ã¥Á oµn°¤ 57 ·Ê¨³Îµ¦» 42 ·Ê·ÁÈ Á°¦r ÁÈrµ¦Îµ¦» ®¨´n°¤Ánµ´74 Á°¦rÁÈrÁÈ Á·49 ¨oµµÂµ¤µ¦µ-1 µ¦µ-1 ¦³ª´·µ¦n°¤°³Å®¨n¸ÉµÎ µAISI 4340 ¨³µ¦Îµ¦» µµ¦n°¤ ¸É 1 2 ¦µ¥µ¦°³Å®¨n ®¤µ¥Á¨ °³Å®¨n ®¤µ¥Á¨ ¸É ¸ÉÁ oµn°¤ ¦oµª Final drive shaft 01 02 03 05 06 05 06 08 11 16 07 08 09 10 11 12 15 16 17 18 19 20 23 24 Final drive gear 01 02 03 01 02 03 3 Final drive pinion 4 Second reduction shaft Shipper shaft pinion Swing shaft 5 6 εª 02 04 05 06 07 08 09 10 12 14 15 19 20 21 22 16 17 05 20 21 26 30 32 07 08 21 22 23 25 26 27 30 32 35 37 57 ·Ê 08 09 10 12 14 ®¤µ¥Á¨ ¸É µ 01 02 03 07 09 10 15 18 19 4,685,112 02 03 04 05 06 07 15 16 17 07 08 17 ·Ê ¦ª¤Á·¼ Á¸ ¥µµ¦Îµ¦» εªÁ·¸É ¼ Á¸ ¥ (µ) 13,729,184 22,224,000 1,140,000 05 20 21 30 32 3,361,940 25 32 35 37 3,900,000 25 ·Ê 49,040,236 99 £µª µ¦ª·Á¦µ³®rµÁ«¦¬«µ¦r °·Ên ª¸Én°¤Ã¥¨µ¦ª·¥´ 100 °³Å®¨n ¸ÉÁÈ ·Ên ªÁ¦ºÉ °´¦¨Ã¥´ªÉ Ŧ· ¬´ ¼o ¨·³Îµ®°µ¥»µ¦Äoµ (Expected life) Ân¨³¦´ÊŪo¹É ¦· ¬´ ¼°o °Â³¤¸ °o ¤¼¨nµÇ¸ÉÄoµÎ ®°µ¥»Án o°¤¼¨µ¦ °°Â¦³ª´·µ¦Äoµ °Á¦ºÉ °´¦´ªÉ 訳¨µ¦Äo°³Å®¨n¸É µ¥Ä®oÂnļ o oÁ¦ºÉ °´ ¦¹É n ªÄ®nµ¦Îµ®´ªÉ äÄoµ¤¸ªµ¤Â¤n¥Îµn° oµ¼ ¹É Á¤ºÉ°¹Áª¨µµ¼Äo oµÁ¦ºÉ °´¦ÈµÎ °³Å®¨nª´ Ä®¤nÁ oµÁ¨¸É¥Â´ªÁnµÎµÄ®oªµ¤¤´É °¦³¸ Ê ¹Ân ³Á¸¥ª´nµÄonµ¥Äµ¦ Á¨¸É¥°³Å®¨nȤ¸nµ¼ Án´ Ä ³¸Éµ¦ÎµÁ·µ¦ª·¥´ o°¤¼ ¨»Â¦Á¦ºÉ °µ¦®µªµ¤Â Ȧ ¨oµÅoÁ¦È ¨µ¼ªo · ¥´ ¤¸ªµ¤¤´É Īnµ¨¸ÉÅonµ³¤¸ªµ¤¼o°Äªµ¸ÉÅoµ¨µ¦ª·¥´ ¹ n ¤° o°¤¼¨Ä®o®nª¥µ¼¦o ´·° °µ¦Å¢¢o µÅoµÎ µ¦Îµ°³Å®¨nÁnµ¸É¥» £µ¡Â¨oªÎµª ®¹ÉεÁ·µ¦n°¤µ¤¦¦¤ª·¸Ä®¤n¸ÉÅoµ µ¦ª·¥´ ¹É °³Å®¨nnª®¹É¼Îµ ¹ÊÄoµÂ¨oªÂ¨³ ·µ¤µ¦Äoµ°¥nµÄ¨o·´ »´ n ª®¹Éε¨´ÎµÁ·µ¦n°¤Â¨³n ª¸Én°¤Á¦È ¦°ÁÈ °³Å®¨nµÎ ¦°ÎµÄ®oÁ·ªµ¤¤´É ¹ÊĦ³¼ µ¦µ.1 ¦µ¥µ¦¦µµnµÄonµ¥Â¨³°µ¥» °°³Å®¨n¸ÉµÎ ®Ã¥¦· ¬´ ¼o ¨· ¸É ¦µ¥µ¦°³Å®¨n ¦µµ(µ) °µ¥»Äoµ (´ªÉ ä) 1 2 3 4 5 6 Final drive shaft Final drive gear Final drive pinion Shipper shaft Shipper shaft pinion Swing shaft 980,565 1,561,704 1,852,000 2,206,495 1,300,000 650,000 33,000 35,000 33,000 20,000 20,000 20,000 nµÄoµ°³Å®¨n (µ/´ªÉ 䵦 εµ) 28.02 44.62 56.12 110.32 65 32.5 101 £µª µ¦ª·Á¦µ³®rµ¦°¥Îµ¨´°o°¥¸É» 102 µ¦ª·Á¦µ³®rµ¦°¥ (Regression analysis) ÁÈ ª·¸µ¦µ··¸ÉÄoĵ¦ ª·Á¦µ³®r °o ¤¼¨Â¨³¦oµªµ¤´¤¡´r °´ªÂ¦¸ÉÄ®oªµ¤ÄÁ¡ºÉ°¸É³Îµµ¥Â¨³¦³¤µnµ ªÃo¤ ° o°¤¼¨ª·¸µ¦¸É·¥¤¤µ¸É»º°µ¦¦³¤µnµoª¥ª·¸µÎ ¨´°o°¥¸É» (Least square method) ´´ª°¥nµµ¦ª·Á¦µ³®r´ ¸Ê .1 µ¦®µ¤µ¦°µ¥»ªµ¤Áo ¨o µ ¤µ¦µ¦ª·Á¦µ³®r®µ°µ¥» °ª´»¸É¦´ªµ¤Áo¨oµÃ¥´ªÉ ųÄo¤µ¦ °Basquin Ä µ¦ª·Á¦µ³®r V R = A 1 BR (.1) Än log ´Ê°oµ¤µ¦(.1) logV R = log $ % log1 R (.2) ¹Éº°¤µ¦Áo¦Ä¦µ¢¨°-¨°µ¦¹ ¹¤nª¸É2 °µ¦Á·Ã¹É Á ¸¥Ä®¤nÅoåε®´ª ¦Į¤n´ ¸Ê Y = aX + b Á¤ºÉ° Y = log V R a=B b = log A ¨³nµa ¨³b ¸ÉµÎ Ä®o¤¸ªµ¤·¡¨µÎµ¨´°o°¥¸É» ° o°¤¼¨n º° (.3) 103 a= (σ () ݅ ݔσ ) ݅ ݕ ݊ 2 (σ ) ݅ ݔ σ ݅ ݔ2 െ ݊ σ ݅ݕ ݅ݔെ (.4) ഥ aX ഥ b=Y (.5) o°¤¼¨Â¨³¨µ¦¦³´ o°¤¼¨µ¦°ªµ¤Â Ȧ¨oµ °·Ê°´n°Å¸Ê µ¦µ.1 µ¦¦³´ o°¤¼¨µ¦°ªµ¤¨oµ °Á®¨È¨oµ¤Îɵ¦¹¼ AISI 4340 AISI4340 n=4 sum life x 435,609 85,546 13,025 11,831 stress y 400 600 700 800 x~=logx y~=logy (x~)2 (y~)2 (x~y~) 5.639097 2.60206 31.79941 6.770716 14.67327 4.9322 2.778151 24.32659 7.718124 13.7024 4.114778 2.845098 16.9314 8.094583 11.70695 4.073021 2.90309 16.5895 8.427931 11.82435 546011 2500 18.7591 11.1284 89.64691 31.01135 51.90696 a = 903.2 b = -0.16919 Åo¤µ¦ (.6) 宦´Îµµ¥°µ¥»µ¦Äoµ °Á¡¨µª·ÁºÊ°Á®¨È¨oµ¤Îɵ¦¹¼ AISI 4340 ´Â 1 logV log 903.2 1 10 0.16919 (.6) 104 Alternating Stress(MPa) Curve Fitting AISI 4340 900 800 700 600 500 400 300 200 100 0 y = 3763.3x-0.169 R² = 0.9372 1,000 10,000 100,000 1,000,000 Loading Cycle (N) ¦¼ .1 S-N Curve °Á®¨È¨oµÂ¦¹¼ AISI 4340 ¸Éµn µ¦¦³´ o°¤¼¨Â¨oª µ¦µ.2 µ¦¦³´ o°¤¼¨µ¦°ªµ¤¨oµ °·Ê°ÁºÊ°ÁºÉ°¤Åo¢¨´r FCAW n=7 sum life x 6,713,160 1,467,630 804,931 105,401 216,760 51,210 1,710 stress y 300 350 400 500 600 700 800 x~=logx 6.826927 6.166617 5.905759 5.022845 5.335979 4.709355 3.232996 y~=logy 2.477121 2.544068 2.60206 2.69897 2.778151 2.845098 2.90309 (x~)2 46.60693 38.02716 34.87799 25.22897 28.47267 22.17802 10.45226 (y~)2 6.13613 6.472282 6.770716 7.284439 7.718124 8.094583 8.427931 (x~y~) 16.91113 15.68829 15.36714 13.55651 14.82416 13.39858 9.385679 9,360,802 3,650 37 19 206 51 99 a = 560.9 b = -0.12721 105 Åo¤µ¦ (.7) 宦´Îµµ¥°µ¥»µ¦Äoµ °Á¡¨µª·ÁºÊ°Á®¨È¨oµ¤Îɵ¦¹¼ AISI 4340 ÁºÉ°¤¡°oª¥ÁºÊ°ÁºÉ°¤Åo¢¨´r ´  1 10 1 logV log 560.9 0.12721 (.7) Alternating Stress(MPa) Curve Fitting FCAW 1000 900 800 700 600 500 400 300 200 100 0 y = 2337.1x-0.127 R² = 0.8696 1,000 10,000 100,000 1,000,000 Loading Cycle(N) ¦¼ .2 S-N Curve °ÁºÊ°ÁºÉ°¤Åo¢¨´r¸Éµn µ¦¦³´ o°¤¼¨Â¨oª µ¦µ.3 µ¦¦³´ o°¤¼¨µ¦°ªµ¤¨oµ °·Ê°ÁºÊ°ÁºÉ°¤Â¤ MAG n=4 sum life x 1,582,570 202,039 39,854 3,663 1,828,126 stress y 350 400 500 600 x~=logx y~=logy (x~)2 (y~)2 (x~y~) 6.199363 2.544068 38.4321 6.472282 15.7716 5.305435 2.60206 28.14764 6.770716 13.80506 4.600472 2.69897 21.16434 7.284439 12.41654 3.563837 2.778151 12.70093 7.718124 9.900878 1850 19.66911 10.62325 100.445 28.24556 51.89408 106 a = 308.4 b = -0.09214 Åo¤µ¦ (.8) 宦´Îµµ¥°µ¥»µ¦Äoµ °Á¡¨µª·ÁºÊ°Á®¨È¨oµ¤Îɵ¦¹¼ AISI 4340 ÁºÉ°¤¡°oª¥ÁºÊ°ÁºÉ°¤Â¤´Â 1 logV log 308.4 (.8) 1 10 0.09214 Curve Fitting MAG 700 Alternating Stress(MPa) 600 500 400 y = 1285x-0.092 R² = 0.9825 300 200 100 0 1,000 10,000 100,000 1,000,000 10,000,000 Loading Cycle(N) ¦¼ .3 S-N Curve °ÁºÊ°ÁºÉ°¤Â¤ ¸Éµn µ¦¦³´ o°¤¼¨Â¨oª 107 µ¦µ.4 µ¦¦³´ o°¤¼¨µ¦°ªµ¤¨oµ °·Ê°ÁºÊ°ÁºÉ°¤®» ¤o ¢¨´r SMAW n=5 sum life x 1,166,063 203,481 86,168 52,474 4,270 stress y 350 400 500 600 700 1,512,456 x~=logx y~=logy (x~)2 (y~)2 (x~y~) 6.066722 2.544068 36.80512 6.472282 15.43415 5.308524 2.60206 28.18043 6.770716 13.8131 4.935346 2.69897 24.35764 7.284439 13.32035 4.719944 2.778151 22.27787 7.718124 13.11272 3.630428 2.845098 13.18001 8.094583 10.32892 2550 24.66096 13.46835 124.8011 36.34014 66.00924 a = 532.7 ¨³b = -0.13232 Åo¤µ¦ (.8) 宦´Îµµ¥°µ¥»µ¦Äoµ °Á¡¨µª·ÁºÊ°Á®¨È¨oµ¤Îɵ¦¹¼ AISI 4340 ÁºÉ°¤¡°oª¥ÁºÊ°ÁºÉ°¤Â¤´Â 1 logV log 308.4 (.8) 1 10 0.09214 Alternating Stress(MPa) Curve Fitting SMAW 800 600 y = 2219.7x-0.132 R² = 0.9114 400 200 0 1,000 10,000 100,000 1,000,000 Loading Cycle(N) ¦¼ .4 S-N Curve °ÁºÊ°ÁºÉ°¤®» ¤o ¢¨´r¸Éµn µ¦¦³´ o°¤¼¨Â¨oª 108 £µª ´Ê°µ¦®µÂ¢Á°¦r ¦´¦» nµªµ¤¨oµ 109 ¢Á°¦r ¦´¦» nµªµ¤Â Ȧ¨oµµ¤Marine equation Se x Ka º°Â¢Á°¦r¦´¦» ·ª®µÅoµ¤µ¦ K a Kb Kc K d Ke K f Se ' ÁÈ ´n°Å¸Ê asutb Ka 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FATIGUE LIFE ASSESSMENT OF WELD SURFACING OF AISI 4340. The 2nd SOUTH-EAST ASIA INTERNATIONAL WELDING CONGRESS (section6 Design &Fabrication). 25-26 February 2010 Bangkok, Thailand. Paper NO 52, Page 467-471.