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Influence of Process Parameters on Laser Shock Processing Effect of Aero-Engine Blades
Aero-engine is the core component of the aircraft, and the blade is the key part of the engine. Because the blade is exposed to the harsh environment of high temperature, high pressure, and complex stress coupling for a long time, it is very prone to fracture failure. Laser shock processing is an ad...
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Published in: | Surface investigation, x-ray, synchrotron and neutron techniques x-ray, synchrotron and neutron techniques, 2022-12, Vol.16 (6), p.1208-1220 |
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creator | Mengyue Wang Konovalov, Sergey Dai, Fengze Chen, Xizhang |
description | Aero-engine is the core component of the aircraft, and the blade is the key part of the engine. Because the blade is exposed to the harsh environment of high temperature, high pressure, and complex stress coupling for a long time, it is very prone to fracture failure. Laser shock processing is an advanced surface strengthening technology. It is widely used in the surface strengthening treatment of aero-engine blades because of its technical advantages such as strong controllability, good applicability, and good strengthening effect. This paper mainly expounds on the development history of laser shock processing technology and makes a brief analysis of its development prospects and existing problems. Focusing on the laser process parameters, absorption layer and constraint layer, contact film, etc., the influence of process parameters on the strengthening effect of laser shock aero-engine blades is analyzed. It lays a theoretical foundation for selecting reasonable process parameters in the laser shock processing test and practical application in the future and is of great significance to obtain the best effect of laser shock processing. |
doi_str_mv | 10.1134/S102745102206043X |
format | article |
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Because the blade is exposed to the harsh environment of high temperature, high pressure, and complex stress coupling for a long time, it is very prone to fracture failure. Laser shock processing is an advanced surface strengthening technology. It is widely used in the surface strengthening treatment of aero-engine blades because of its technical advantages such as strong controllability, good applicability, and good strengthening effect. This paper mainly expounds on the development history of laser shock processing technology and makes a brief analysis of its development prospects and existing problems. Focusing on the laser process parameters, absorption layer and constraint layer, contact film, etc., the influence of process parameters on the strengthening effect of laser shock aero-engine blades is analyzed. It lays a theoretical foundation for selecting reasonable process parameters in the laser shock processing test and practical application in the future and is of great significance to obtain the best effect of laser shock processing.</description><identifier>ISSN: 1027-4510</identifier><identifier>EISSN: 1819-7094</identifier><identifier>DOI: 10.1134/S102745102206043X</identifier><language>eng</language><publisher>Moscow: Pleiades Publishing</publisher><subject>Aerospace engines ; Blades ; Chemistry and Materials Science ; High temperature ; Laser shock processing ; Lasers ; Materials Science ; Process parameters ; Strengthening ; Surfaces and Interfaces ; Thin Films</subject><ispartof>Surface investigation, x-ray, synchrotron and neutron techniques, 2022-12, Vol.16 (6), p.1208-1220</ispartof><rights>Pleiades Publishing, Ltd. 2022. ISSN 1027-4510, Journal of Surface Investigation: X-ray, Synchrotron and Neutron Techniques, 2022, Vol. 16, No. 6, pp. 1208–1220. © Pleiades Publishing, Ltd., 2022.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c316t-2b74ed65a7c465efdfdc324c54d764701b32a6f1f922391ffb462e79979747863</citedby><cites>FETCH-LOGICAL-c316t-2b74ed65a7c465efdfdc324c54d764701b32a6f1f922391ffb462e79979747863</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27922,27923</link.rule.ids></links><search><creatorcontrib>Mengyue Wang</creatorcontrib><creatorcontrib>Konovalov, Sergey</creatorcontrib><creatorcontrib>Dai, Fengze</creatorcontrib><creatorcontrib>Chen, Xizhang</creatorcontrib><title>Influence of Process Parameters on Laser Shock Processing Effect of Aero-Engine Blades</title><title>Surface investigation, x-ray, synchrotron and neutron techniques</title><addtitle>J. Surf. Investig</addtitle><description>Aero-engine is the core component of the aircraft, and the blade is the key part of the engine. Because the blade is exposed to the harsh environment of high temperature, high pressure, and complex stress coupling for a long time, it is very prone to fracture failure. Laser shock processing is an advanced surface strengthening technology. It is widely used in the surface strengthening treatment of aero-engine blades because of its technical advantages such as strong controllability, good applicability, and good strengthening effect. This paper mainly expounds on the development history of laser shock processing technology and makes a brief analysis of its development prospects and existing problems. Focusing on the laser process parameters, absorption layer and constraint layer, contact film, etc., the influence of process parameters on the strengthening effect of laser shock aero-engine blades is analyzed. It lays a theoretical foundation for selecting reasonable process parameters in the laser shock processing test and practical application in the future and is of great significance to obtain the best effect of laser shock processing.</description><subject>Aerospace engines</subject><subject>Blades</subject><subject>Chemistry and Materials Science</subject><subject>High temperature</subject><subject>Laser shock processing</subject><subject>Lasers</subject><subject>Materials Science</subject><subject>Process parameters</subject><subject>Strengthening</subject><subject>Surfaces and Interfaces</subject><subject>Thin Films</subject><issn>1027-4510</issn><issn>1819-7094</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2022</creationdate><recordtype>article</recordtype><recordid>eNp1kE9LAzEQxYMoWKsfwFvA82r-pznWUrVQsFAVb0uandTWNqnJ7sFvb0oVD-JlZuD93ht4CF1Sck0pFzdzSpgWskxGFBH89Qj16ICaShMjjstd5Gqvn6KznNeESM2l6qGXSfCbDoIDHD2epeggZzyzyW6hhZRxDHhqMyQ8f4vu_YdYhSUeew-u3duGkGI1DstVAHy7sQ3kc3Ti7SbDxffuo-e78dPooZo-3k9Gw2nlOFVtxRZaQKOk1U4oCb7xjeNMOCkarYQmdMGZVZ56wxg31PuFUAy0MdpooQeK99HVIXeX4kcHua3XsUuhvKyZllwZSrgsFD1QLsWcE_h6l1Zbmz5rSup9ffWf-oqHHTy5sGEJ6Tf5f9MXngVwBw</recordid><startdate>20221201</startdate><enddate>20221201</enddate><creator>Mengyue Wang</creator><creator>Konovalov, Sergey</creator><creator>Dai, Fengze</creator><creator>Chen, Xizhang</creator><general>Pleiades Publishing</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope></search><sort><creationdate>20221201</creationdate><title>Influence of Process Parameters on Laser Shock Processing Effect of Aero-Engine Blades</title><author>Mengyue Wang ; Konovalov, Sergey ; Dai, Fengze ; Chen, Xizhang</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c316t-2b74ed65a7c465efdfdc324c54d764701b32a6f1f922391ffb462e79979747863</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2022</creationdate><topic>Aerospace engines</topic><topic>Blades</topic><topic>Chemistry and Materials Science</topic><topic>High temperature</topic><topic>Laser shock processing</topic><topic>Lasers</topic><topic>Materials Science</topic><topic>Process parameters</topic><topic>Strengthening</topic><topic>Surfaces and Interfaces</topic><topic>Thin Films</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Mengyue Wang</creatorcontrib><creatorcontrib>Konovalov, Sergey</creatorcontrib><creatorcontrib>Dai, Fengze</creatorcontrib><creatorcontrib>Chen, Xizhang</creatorcontrib><collection>CrossRef</collection><jtitle>Surface investigation, x-ray, synchrotron and neutron techniques</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Mengyue Wang</au><au>Konovalov, Sergey</au><au>Dai, Fengze</au><au>Chen, Xizhang</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Influence of Process Parameters on Laser Shock Processing Effect of Aero-Engine Blades</atitle><jtitle>Surface investigation, x-ray, synchrotron and neutron techniques</jtitle><stitle>J. Surf. Investig</stitle><date>2022-12-01</date><risdate>2022</risdate><volume>16</volume><issue>6</issue><spage>1208</spage><epage>1220</epage><pages>1208-1220</pages><issn>1027-4510</issn><eissn>1819-7094</eissn><abstract>Aero-engine is the core component of the aircraft, and the blade is the key part of the engine. Because the blade is exposed to the harsh environment of high temperature, high pressure, and complex stress coupling for a long time, it is very prone to fracture failure. Laser shock processing is an advanced surface strengthening technology. It is widely used in the surface strengthening treatment of aero-engine blades because of its technical advantages such as strong controllability, good applicability, and good strengthening effect. This paper mainly expounds on the development history of laser shock processing technology and makes a brief analysis of its development prospects and existing problems. Focusing on the laser process parameters, absorption layer and constraint layer, contact film, etc., the influence of process parameters on the strengthening effect of laser shock aero-engine blades is analyzed. It lays a theoretical foundation for selecting reasonable process parameters in the laser shock processing test and practical application in the future and is of great significance to obtain the best effect of laser shock processing.</abstract><cop>Moscow</cop><pub>Pleiades Publishing</pub><doi>10.1134/S102745102206043X</doi><tpages>13</tpages></addata></record> |
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subjects | Aerospace engines Blades Chemistry and Materials Science High temperature Laser shock processing Lasers Materials Science Process parameters Strengthening Surfaces and Interfaces Thin Films |
title | Influence of Process Parameters on Laser Shock Processing Effect of Aero-Engine Blades |
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