Manufacturing of Ni-based superalloy thin-walled components by complex strain-path spinning combined with solution heat treatment
Complex thin-walled components, such as conical-cylindrical parts, widely used in combustor shells, are generally made of Ni-based superalloy. However, it is difficult to manufacture the complex components with high dimensional accuracy by single process, and the formability of Ni-based superalloy i...
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Veröffentlicht in: | International journal of advanced manufacturing technology 2021-11, Vol.117 (1-2), p.199-215 |
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description | Complex thin-walled components, such as conical-cylindrical parts, widely used in combustor shells, are generally made of Ni-based superalloy. However, it is difficult to manufacture the complex components with high dimensional accuracy by single process, and the formability of Ni-based superalloy is limited at room temperature due to the severe work hardening. A new spinning-heat treatment composite forming method of manufacturing the conical-cylindrical parts, consisting of shear spinning, solution heat treatment, and deep drawing spinning, was proposed. The feasibility of manufacturing the Ni-based superalloy complex component at room temperature was explored, and the spinning formability under complex strain path was analyzed. The results show that the limited thinning ratio of Ni-based superalloy is about 50% at room temperature under the strain state of pure shear deformation, and the work hardening of conical pre-formed blank can be completely eliminated by a 1200°C × 20 min solution heat treatment. Wrinkling occurs easily when single-pass deep drawing spinning was adopted to form the cylindrical section with the spinning coefficient of 0.78 under the linear strain path. Fracture along axial direction occurs easily at the opening area of the spun workpiece under the locally serrated strain path when multi-pass deep drawing spinning was adopted to form the cylindrical section without solution heat treatment. The spinning formability of the Ni-based superalloy of the multi-pass deep drawing spinning improves remarkably after solution heat treatment due to the improvement of deformation uniformity and the significant decrease of the tangential compressive stress at flange area. The experiments were carried out to verify the theoretical analysis results, and the Ni-based superalloy conical-cylindrical parts with high dimensional accuracy were manufactured successfully by the developed method combining of shear spinning followed by a solution heat treatment and multi-pass deep drawing spinning. |
doi_str_mv | 10.1007/s00170-021-07676-1 |
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However, it is difficult to manufacture the complex components with high dimensional accuracy by single process, and the formability of Ni-based superalloy is limited at room temperature due to the severe work hardening. A new spinning-heat treatment composite forming method of manufacturing the conical-cylindrical parts, consisting of shear spinning, solution heat treatment, and deep drawing spinning, was proposed. The feasibility of manufacturing the Ni-based superalloy complex component at room temperature was explored, and the spinning formability under complex strain path was analyzed. The results show that the limited thinning ratio of Ni-based superalloy is about 50% at room temperature under the strain state of pure shear deformation, and the work hardening of conical pre-formed blank can be completely eliminated by a 1200°C × 20 min solution heat treatment. Wrinkling occurs easily when single-pass deep drawing spinning was adopted to form the cylindrical section with the spinning coefficient of 0.78 under the linear strain path. Fracture along axial direction occurs easily at the opening area of the spun workpiece under the locally serrated strain path when multi-pass deep drawing spinning was adopted to form the cylindrical section without solution heat treatment. The spinning formability of the Ni-based superalloy of the multi-pass deep drawing spinning improves remarkably after solution heat treatment due to the improvement of deformation uniformity and the significant decrease of the tangential compressive stress at flange area. The experiments were carried out to verify the theoretical analysis results, and the Ni-based superalloy conical-cylindrical parts with high dimensional accuracy were manufactured successfully by the developed method combining of shear spinning followed by a solution heat treatment and multi-pass deep drawing spinning.</description><identifier>ISSN: 0268-3768</identifier><identifier>EISSN: 1433-3015</identifier><identifier>DOI: 10.1007/s00170-021-07676-1</identifier><language>eng</language><publisher>London: Springer London</publisher><subject>CAE) and Design ; Combustion chambers ; Compressive properties ; Computer-Aided Engineering (CAD ; Deep drawing ; Engineering ; Formability ; Heat treating ; Industrial and Production Engineering ; Manufacturing ; Mechanical Engineering ; Media Management ; Nickel base alloys ; Original Article ; Production methods ; Room temperature ; Shear deformation ; Solution heat treatment ; Spinning (metals) ; Strain analysis ; Superalloys ; Tempering ; Work hardening ; Workpieces</subject><ispartof>International journal of advanced manufacturing technology, 2021-11, Vol.117 (1-2), p.199-215</ispartof><rights>The Author(s), under exclusive licence to Springer-Verlag London Ltd., part of Springer Nature 2021</rights><rights>The Author(s), under exclusive licence to Springer-Verlag London Ltd., part of Springer Nature 2021.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c319t-b1b39b3c846c4692c9ed6290d854c6017496b817480ccc206f088254e245df0a3</citedby><cites>FETCH-LOGICAL-c319t-b1b39b3c846c4692c9ed6290d854c6017496b817480ccc206f088254e245df0a3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://link.springer.com/content/pdf/10.1007/s00170-021-07676-1$$EPDF$$P50$$Gspringer$$H</linktopdf><linktohtml>$$Uhttps://link.springer.com/10.1007/s00170-021-07676-1$$EHTML$$P50$$Gspringer$$H</linktohtml><link.rule.ids>314,776,780,27903,27904,41467,42536,51298</link.rule.ids></links><search><creatorcontrib>Xiao, Gangfeng</creatorcontrib><creatorcontrib>Xia, Qinxiang</creatorcontrib><creatorcontrib>Zhang, Yilong</creatorcontrib><creatorcontrib>Cheng, Xiuquan</creatorcontrib><title>Manufacturing of Ni-based superalloy thin-walled components by complex strain-path spinning combined with solution heat treatment</title><title>International journal of advanced manufacturing technology</title><addtitle>Int J Adv Manuf Technol</addtitle><description>Complex thin-walled components, such as conical-cylindrical parts, widely used in combustor shells, are generally made of Ni-based superalloy. However, it is difficult to manufacture the complex components with high dimensional accuracy by single process, and the formability of Ni-based superalloy is limited at room temperature due to the severe work hardening. A new spinning-heat treatment composite forming method of manufacturing the conical-cylindrical parts, consisting of shear spinning, solution heat treatment, and deep drawing spinning, was proposed. The feasibility of manufacturing the Ni-based superalloy complex component at room temperature was explored, and the spinning formability under complex strain path was analyzed. The results show that the limited thinning ratio of Ni-based superalloy is about 50% at room temperature under the strain state of pure shear deformation, and the work hardening of conical pre-formed blank can be completely eliminated by a 1200°C × 20 min solution heat treatment. Wrinkling occurs easily when single-pass deep drawing spinning was adopted to form the cylindrical section with the spinning coefficient of 0.78 under the linear strain path. Fracture along axial direction occurs easily at the opening area of the spun workpiece under the locally serrated strain path when multi-pass deep drawing spinning was adopted to form the cylindrical section without solution heat treatment. The spinning formability of the Ni-based superalloy of the multi-pass deep drawing spinning improves remarkably after solution heat treatment due to the improvement of deformation uniformity and the significant decrease of the tangential compressive stress at flange area. The experiments were carried out to verify the theoretical analysis results, and the Ni-based superalloy conical-cylindrical parts with high dimensional accuracy were manufactured successfully by the developed method combining of shear spinning followed by a solution heat treatment and multi-pass deep drawing spinning.</description><subject>CAE) and Design</subject><subject>Combustion chambers</subject><subject>Compressive properties</subject><subject>Computer-Aided Engineering (CAD</subject><subject>Deep drawing</subject><subject>Engineering</subject><subject>Formability</subject><subject>Heat treating</subject><subject>Industrial and Production Engineering</subject><subject>Manufacturing</subject><subject>Mechanical Engineering</subject><subject>Media Management</subject><subject>Nickel base alloys</subject><subject>Original Article</subject><subject>Production methods</subject><subject>Room temperature</subject><subject>Shear deformation</subject><subject>Solution heat treatment</subject><subject>Spinning (metals)</subject><subject>Strain analysis</subject><subject>Superalloys</subject><subject>Tempering</subject><subject>Work hardening</subject><subject>Workpieces</subject><issn>0268-3768</issn><issn>1433-3015</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2021</creationdate><recordtype>article</recordtype><sourceid>AFKRA</sourceid><sourceid>BENPR</sourceid><sourceid>CCPQU</sourceid><sourceid>DWQXO</sourceid><recordid>eNp9kEtPxCAUhYnRxHH0D7gicY3yaCldmomvZNSNrgllqMOkAxVoxln6z6VTE3duuHDvOYfcD4BLgq8JxtVNxJhUGGFKEK54xRE5AjNSMIYYJuUxmGHKBWIVF6fgLMZNlnPCxQx8Pys3tEqnIVj3AX0LXyxqVDQrGIfeBNV1fg_T2jq0y_fc1n7be2dcirDZH16d-YIxBZU1vUprGHvr3JiWh4112bOzY9t3Q7LewbVRCaaQz22OOQcnreqiufitc_B-f_e2eETL14enxe0SaUbqhBrSsLphWhRcF7ymujYrTmu8EmWhed6-qHkjchFYa00xb7EQtCwMLcpVixWbg6sptw_-czAxyY0fgstfSlpWtagYrUlW0Umlg48xmFb2wW5V2EuC5YhaTqhlRi0PqOVoYpMp9iNFE_6i_3H9AIVTg30</recordid><startdate>20211101</startdate><enddate>20211101</enddate><creator>Xiao, Gangfeng</creator><creator>Xia, Qinxiang</creator><creator>Zhang, Yilong</creator><creator>Cheng, Xiuquan</creator><general>Springer London</general><general>Springer Nature B.V</general><scope>AAYXX</scope><scope>CITATION</scope><scope>8FE</scope><scope>8FG</scope><scope>ABJCF</scope><scope>AFKRA</scope><scope>BENPR</scope><scope>BGLVJ</scope><scope>CCPQU</scope><scope>DWQXO</scope><scope>HCIFZ</scope><scope>L6V</scope><scope>M7S</scope><scope>PQEST</scope><scope>PQQKQ</scope><scope>PQUKI</scope><scope>PRINS</scope><scope>PTHSS</scope></search><sort><creationdate>20211101</creationdate><title>Manufacturing of Ni-based superalloy thin-walled components by complex strain-path spinning combined with solution heat treatment</title><author>Xiao, Gangfeng ; Xia, Qinxiang ; Zhang, Yilong ; Cheng, Xiuquan</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c319t-b1b39b3c846c4692c9ed6290d854c6017496b817480ccc206f088254e245df0a3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2021</creationdate><topic>CAE) and Design</topic><topic>Combustion chambers</topic><topic>Compressive properties</topic><topic>Computer-Aided Engineering (CAD</topic><topic>Deep drawing</topic><topic>Engineering</topic><topic>Formability</topic><topic>Heat treating</topic><topic>Industrial and Production Engineering</topic><topic>Manufacturing</topic><topic>Mechanical Engineering</topic><topic>Media Management</topic><topic>Nickel base alloys</topic><topic>Original Article</topic><topic>Production methods</topic><topic>Room temperature</topic><topic>Shear deformation</topic><topic>Solution heat treatment</topic><topic>Spinning (metals)</topic><topic>Strain analysis</topic><topic>Superalloys</topic><topic>Tempering</topic><topic>Work hardening</topic><topic>Workpieces</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Xiao, Gangfeng</creatorcontrib><creatorcontrib>Xia, Qinxiang</creatorcontrib><creatorcontrib>Zhang, Yilong</creatorcontrib><creatorcontrib>Cheng, Xiuquan</creatorcontrib><collection>CrossRef</collection><collection>ProQuest SciTech Collection</collection><collection>ProQuest Technology Collection</collection><collection>Materials Science & Engineering Collection</collection><collection>ProQuest Central UK/Ireland</collection><collection>ProQuest Central</collection><collection>Technology Collection</collection><collection>ProQuest One Community College</collection><collection>ProQuest Central</collection><collection>SciTech Premium Collection</collection><collection>ProQuest Engineering Collection</collection><collection>Engineering Database</collection><collection>ProQuest One Academic Eastern Edition (DO NOT USE)</collection><collection>ProQuest One Academic</collection><collection>ProQuest One Academic UKI Edition</collection><collection>ProQuest Central China</collection><collection>Engineering collection</collection><jtitle>International journal of advanced manufacturing technology</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Xiao, Gangfeng</au><au>Xia, Qinxiang</au><au>Zhang, Yilong</au><au>Cheng, Xiuquan</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Manufacturing of Ni-based superalloy thin-walled components by complex strain-path spinning combined with solution heat treatment</atitle><jtitle>International journal of advanced manufacturing technology</jtitle><stitle>Int J Adv Manuf Technol</stitle><date>2021-11-01</date><risdate>2021</risdate><volume>117</volume><issue>1-2</issue><spage>199</spage><epage>215</epage><pages>199-215</pages><issn>0268-3768</issn><eissn>1433-3015</eissn><abstract>Complex thin-walled components, such as conical-cylindrical parts, widely used in combustor shells, are generally made of Ni-based superalloy. However, it is difficult to manufacture the complex components with high dimensional accuracy by single process, and the formability of Ni-based superalloy is limited at room temperature due to the severe work hardening. A new spinning-heat treatment composite forming method of manufacturing the conical-cylindrical parts, consisting of shear spinning, solution heat treatment, and deep drawing spinning, was proposed. The feasibility of manufacturing the Ni-based superalloy complex component at room temperature was explored, and the spinning formability under complex strain path was analyzed. The results show that the limited thinning ratio of Ni-based superalloy is about 50% at room temperature under the strain state of pure shear deformation, and the work hardening of conical pre-formed blank can be completely eliminated by a 1200°C × 20 min solution heat treatment. Wrinkling occurs easily when single-pass deep drawing spinning was adopted to form the cylindrical section with the spinning coefficient of 0.78 under the linear strain path. Fracture along axial direction occurs easily at the opening area of the spun workpiece under the locally serrated strain path when multi-pass deep drawing spinning was adopted to form the cylindrical section without solution heat treatment. The spinning formability of the Ni-based superalloy of the multi-pass deep drawing spinning improves remarkably after solution heat treatment due to the improvement of deformation uniformity and the significant decrease of the tangential compressive stress at flange area. The experiments were carried out to verify the theoretical analysis results, and the Ni-based superalloy conical-cylindrical parts with high dimensional accuracy were manufactured successfully by the developed method combining of shear spinning followed by a solution heat treatment and multi-pass deep drawing spinning.</abstract><cop>London</cop><pub>Springer London</pub><doi>10.1007/s00170-021-07676-1</doi><tpages>17</tpages></addata></record> |
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subjects | CAE) and Design Combustion chambers Compressive properties Computer-Aided Engineering (CAD Deep drawing Engineering Formability Heat treating Industrial and Production Engineering Manufacturing Mechanical Engineering Media Management Nickel base alloys Original Article Production methods Room temperature Shear deformation Solution heat treatment Spinning (metals) Strain analysis Superalloys Tempering Work hardening Workpieces |
title | Manufacturing of Ni-based superalloy thin-walled components by complex strain-path spinning combined with solution heat treatment |
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