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Improving the fretting and corrosion fatigue performance of 300M ultra-high strength steel using the ultrasonic surface rolling process
300M ultra-high strength steels (300M steels) are frequently used in the manufacture of aircraft landing gear due to their high strength and ductility. However, their high sensitivity to surface defects accelerates fatigue failure and hinders their wider application. In this work, ultrasonic surface...
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Published in: | International journal of fatigue 2019-04, Vol.121, p.30-38 |
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description | 300M ultra-high strength steels (300M steels) are frequently used in the manufacture of aircraft landing gear due to their high strength and ductility. However, their high sensitivity to surface defects accelerates fatigue failure and hinders their wider application. In this work, ultrasonic surface rolling processing (USRP) was used to process 300M steel. The surface roughness, hardness, microstructure, and residual stresses before and after USRP treatment were compared. The surface roughness for USRP-treated samples (0.062 μm) was found to be lower than that for untreated samples (0.32 μm). In addition, a plastically deformed layer was generated on the surface of USRP-treated samples that resulted in higher hardness. Beneficial compressive residual stresses were introduced as a result of USRP treatment. The better surface finish, higher surface hardness and compressive residual stresses lead to significant improvement in the resistance of the 300M steels to fretting fatigue and corrosion fatigue. The fretting fatigue life increased from 11.9 K cycles to 56.3 K cycles, while the corrosion fatigue life increased from 29.9 K cycles to 702.1 K cycles. |
doi_str_mv | 10.1016/j.ijfatigue.2018.11.017 |
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However, their high sensitivity to surface defects accelerates fatigue failure and hinders their wider application. In this work, ultrasonic surface rolling processing (USRP) was used to process 300M steel. The surface roughness, hardness, microstructure, and residual stresses before and after USRP treatment were compared. The surface roughness for USRP-treated samples (0.062 μm) was found to be lower than that for untreated samples (0.32 μm). In addition, a plastically deformed layer was generated on the surface of USRP-treated samples that resulted in higher hardness. Beneficial compressive residual stresses were introduced as a result of USRP treatment. The better surface finish, higher surface hardness and compressive residual stresses lead to significant improvement in the resistance of the 300M steels to fretting fatigue and corrosion fatigue. The fretting fatigue life increased from 11.9 K cycles to 56.3 K cycles, while the corrosion fatigue life increased from 29.9 K cycles to 702.1 K cycles.</description><identifier>ISSN: 0142-1123</identifier><identifier>EISSN: 1879-3452</identifier><identifier>DOI: 10.1016/j.ijfatigue.2018.11.017</identifier><language>eng</language><publisher>Kidlington: Elsevier Ltd</publisher><subject>300M ultra-high strength steels ; Aircraft landing ; Chemical Sciences ; Compressive properties ; Compressive residual stress ; Corrosion ; Corrosion fatigue ; Corrosion resistance ; Crack propagation ; Deformation ; Engineering Sciences ; Fatigue failure ; Fatigue life ; Fretting ; Fretting fatigue ; Hardness ; High strength steels ; Landing gear ; Materials fatigue ; Metal fatigue ; Nickel chromium molybdenum steels ; Residual stress ; Skin pass rolling ; Surface defects ; Surface finish ; Surface hardness ; Surface roughness ; Ultrasonic surface rolling process (USRP)</subject><ispartof>International journal of fatigue, 2019-04, Vol.121, p.30-38</ispartof><rights>2018 Elsevier Ltd</rights><rights>Copyright Elsevier BV Apr 2019</rights><rights>Distributed under a Creative Commons Attribution 4.0 International License</rights><lds50>peer_reviewed</lds50><oa>free_for_read</oa><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c426t-698c1ddc9561b88ff9513066546552b4f8b198673bc749c3285dbd9a21b4ff253</citedby><cites>FETCH-LOGICAL-c426t-698c1ddc9561b88ff9513066546552b4f8b198673bc749c3285dbd9a21b4ff253</cites><orcidid>0000-0001-7919-6904 ; 0000-0002-2546-4464 ; 0000-0003-4083-626X</orcidid></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>230,314,777,781,882,27905,27906</link.rule.ids><backlink>$$Uhttps://univ-rennes.hal.science/hal-01987965$$DView record in HAL$$Hfree_for_read</backlink></links><search><creatorcontrib>Zhao, Weidong</creatorcontrib><creatorcontrib>Liu, Daoxin</creatorcontrib><creatorcontrib>Zhang, Xiaohua</creatorcontrib><creatorcontrib>Zhou, Ying</creatorcontrib><creatorcontrib>Zhang, Ruixia</creatorcontrib><creatorcontrib>Zhang, Hao</creatorcontrib><creatorcontrib>Ye, Chang</creatorcontrib><title>Improving the fretting and corrosion fatigue performance of 300M ultra-high strength steel using the ultrasonic surface rolling process</title><title>International journal of fatigue</title><description>300M ultra-high strength steels (300M steels) are frequently used in the manufacture of aircraft landing gear due to their high strength and ductility. However, their high sensitivity to surface defects accelerates fatigue failure and hinders their wider application. In this work, ultrasonic surface rolling processing (USRP) was used to process 300M steel. The surface roughness, hardness, microstructure, and residual stresses before and after USRP treatment were compared. The surface roughness for USRP-treated samples (0.062 μm) was found to be lower than that for untreated samples (0.32 μm). In addition, a plastically deformed layer was generated on the surface of USRP-treated samples that resulted in higher hardness. Beneficial compressive residual stresses were introduced as a result of USRP treatment. The better surface finish, higher surface hardness and compressive residual stresses lead to significant improvement in the resistance of the 300M steels to fretting fatigue and corrosion fatigue. The fretting fatigue life increased from 11.9 K cycles to 56.3 K cycles, while the corrosion fatigue life increased from 29.9 K cycles to 702.1 K cycles.</description><subject>300M ultra-high strength steels</subject><subject>Aircraft landing</subject><subject>Chemical Sciences</subject><subject>Compressive properties</subject><subject>Compressive residual stress</subject><subject>Corrosion</subject><subject>Corrosion fatigue</subject><subject>Corrosion resistance</subject><subject>Crack propagation</subject><subject>Deformation</subject><subject>Engineering Sciences</subject><subject>Fatigue failure</subject><subject>Fatigue life</subject><subject>Fretting</subject><subject>Fretting fatigue</subject><subject>Hardness</subject><subject>High strength steels</subject><subject>Landing gear</subject><subject>Materials fatigue</subject><subject>Metal fatigue</subject><subject>Nickel chromium molybdenum steels</subject><subject>Residual stress</subject><subject>Skin pass rolling</subject><subject>Surface defects</subject><subject>Surface finish</subject><subject>Surface hardness</subject><subject>Surface roughness</subject><subject>Ultrasonic surface rolling process (USRP)</subject><issn>0142-1123</issn><issn>1879-3452</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2019</creationdate><recordtype>article</recordtype><recordid>eNqFkcFu3CAQhlHVSt2mfYYi5dSDXQYbMMdV1CaRtsolOSOMYRfLazaAV-oT9LWDu2muPQEz3__PMIPQVyA1EODfx9qPTme_X2xNCXQ1QE1AvEMb6ISsmpbR92hDoKUVAG0-ok8pjYQQSQTboD_3x1MMZz_vcT5Y7KLNeX3oecAmxBiSDzN-9ccnG12IRz0bi4PDDSG_8DLlqKuD3x9wytHO-7xerJ3wkv7Z_mVSmL3BaYlOF3kM07SmS3VjU_qMPjg9Jfvl9bxCTz9_PN7cVbuH2_ub7a4yLeW54rIzMAxGMg591zknGTSEc9Zyxmjfuq4H2XHR9Ea00jS0Y0M_SE2h5BxlzRX6dvE96Emdoj_q-FsF7dXddqfWGCl6ITk7Q2GvL2zp8XmxKasxLHEu7SlKoS2QYLRQ4kKZMqwUrXuzBaLWDalRvW1IrRtSAKWMKMrtRWnLh8_eRpWMt2W2g4_WZDUE_1-PF4zGn2Q</recordid><startdate>201904</startdate><enddate>201904</enddate><creator>Zhao, Weidong</creator><creator>Liu, Daoxin</creator><creator>Zhang, Xiaohua</creator><creator>Zhou, Ying</creator><creator>Zhang, Ruixia</creator><creator>Zhang, Hao</creator><creator>Ye, Chang</creator><general>Elsevier Ltd</general><general>Elsevier BV</general><general>Elsevier</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SR</scope><scope>8BQ</scope><scope>8FD</scope><scope>JG9</scope><scope>1XC</scope><scope>VOOES</scope><orcidid>https://orcid.org/0000-0001-7919-6904</orcidid><orcidid>https://orcid.org/0000-0002-2546-4464</orcidid><orcidid>https://orcid.org/0000-0003-4083-626X</orcidid></search><sort><creationdate>201904</creationdate><title>Improving the fretting and corrosion fatigue performance of 300M ultra-high strength steel using the ultrasonic surface rolling process</title><author>Zhao, Weidong ; Liu, Daoxin ; Zhang, Xiaohua ; Zhou, Ying ; Zhang, Ruixia ; Zhang, Hao ; Ye, Chang</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c426t-698c1ddc9561b88ff9513066546552b4f8b198673bc749c3285dbd9a21b4ff253</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2019</creationdate><topic>300M ultra-high strength steels</topic><topic>Aircraft landing</topic><topic>Chemical Sciences</topic><topic>Compressive properties</topic><topic>Compressive residual stress</topic><topic>Corrosion</topic><topic>Corrosion fatigue</topic><topic>Corrosion resistance</topic><topic>Crack propagation</topic><topic>Deformation</topic><topic>Engineering Sciences</topic><topic>Fatigue failure</topic><topic>Fatigue life</topic><topic>Fretting</topic><topic>Fretting fatigue</topic><topic>Hardness</topic><topic>High strength steels</topic><topic>Landing gear</topic><topic>Materials fatigue</topic><topic>Metal fatigue</topic><topic>Nickel chromium molybdenum steels</topic><topic>Residual stress</topic><topic>Skin pass rolling</topic><topic>Surface defects</topic><topic>Surface finish</topic><topic>Surface hardness</topic><topic>Surface roughness</topic><topic>Ultrasonic surface rolling process (USRP)</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Zhao, Weidong</creatorcontrib><creatorcontrib>Liu, Daoxin</creatorcontrib><creatorcontrib>Zhang, Xiaohua</creatorcontrib><creatorcontrib>Zhou, Ying</creatorcontrib><creatorcontrib>Zhang, Ruixia</creatorcontrib><creatorcontrib>Zhang, Hao</creatorcontrib><creatorcontrib>Ye, Chang</creatorcontrib><collection>CrossRef</collection><collection>Engineered Materials Abstracts</collection><collection>METADEX</collection><collection>Technology Research Database</collection><collection>Materials Research Database</collection><collection>Hyper Article en Ligne (HAL)</collection><collection>Hyper Article en Ligne (HAL) (Open Access)</collection><jtitle>International journal of fatigue</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Zhao, Weidong</au><au>Liu, Daoxin</au><au>Zhang, Xiaohua</au><au>Zhou, Ying</au><au>Zhang, Ruixia</au><au>Zhang, Hao</au><au>Ye, Chang</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Improving the fretting and corrosion fatigue performance of 300M ultra-high strength steel using the ultrasonic surface rolling process</atitle><jtitle>International journal of fatigue</jtitle><date>2019-04</date><risdate>2019</risdate><volume>121</volume><spage>30</spage><epage>38</epage><pages>30-38</pages><issn>0142-1123</issn><eissn>1879-3452</eissn><abstract>300M ultra-high strength steels (300M steels) are frequently used in the manufacture of aircraft landing gear due to their high strength and ductility. However, their high sensitivity to surface defects accelerates fatigue failure and hinders their wider application. In this work, ultrasonic surface rolling processing (USRP) was used to process 300M steel. The surface roughness, hardness, microstructure, and residual stresses before and after USRP treatment were compared. The surface roughness for USRP-treated samples (0.062 μm) was found to be lower than that for untreated samples (0.32 μm). In addition, a plastically deformed layer was generated on the surface of USRP-treated samples that resulted in higher hardness. Beneficial compressive residual stresses were introduced as a result of USRP treatment. The better surface finish, higher surface hardness and compressive residual stresses lead to significant improvement in the resistance of the 300M steels to fretting fatigue and corrosion fatigue. The fretting fatigue life increased from 11.9 K cycles to 56.3 K cycles, while the corrosion fatigue life increased from 29.9 K cycles to 702.1 K cycles.</abstract><cop>Kidlington</cop><pub>Elsevier Ltd</pub><doi>10.1016/j.ijfatigue.2018.11.017</doi><tpages>9</tpages><orcidid>https://orcid.org/0000-0001-7919-6904</orcidid><orcidid>https://orcid.org/0000-0002-2546-4464</orcidid><orcidid>https://orcid.org/0000-0003-4083-626X</orcidid><oa>free_for_read</oa></addata></record> |
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subjects | 300M ultra-high strength steels Aircraft landing Chemical Sciences Compressive properties Compressive residual stress Corrosion Corrosion fatigue Corrosion resistance Crack propagation Deformation Engineering Sciences Fatigue failure Fatigue life Fretting Fretting fatigue Hardness High strength steels Landing gear Materials fatigue Metal fatigue Nickel chromium molybdenum steels Residual stress Skin pass rolling Surface defects Surface finish Surface hardness Surface roughness Ultrasonic surface rolling process (USRP) |
title | Improving the fretting and corrosion fatigue performance of 300M ultra-high strength steel using the ultrasonic surface rolling process |
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