Optimization design of variable density lattice structure for additive manufacturing

Lattice material is a kind of super light and high strength porous material with high performance. At present, it is mainly composed of lattice structure with equal density components. In practice, each part of the lattice structure bears different loads, so the performance of the lattice structure...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Veröffentlicht in:Energy (Oxford) 2022-03, Vol.242, p.122554, Article 122554
Hauptverfasser: Zhang, Xinju, Xue, Zhanpu, Cheng, Quntao, Ji, Yunguang
Format: Artikel
Sprache:eng
Schlagworte:
Online-Zugang:Volltext
Tags: Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
container_end_page
container_issue
container_start_page 122554
container_title Energy (Oxford)
container_volume 242
creator Zhang, Xinju
Xue, Zhanpu
Cheng, Quntao
Ji, Yunguang
description Lattice material is a kind of super light and high strength porous material with high performance. At present, it is mainly composed of lattice structure with equal density components. In practice, each part of the lattice structure bears different loads, so the performance of the lattice structure with equal density can not be brought into full play. In view of the above problems, topology optimization was used to the process of lattice structure design to the optimal design of variable density lattice structure. According to the actual load, the optimal variable density lattice structure is designed to achieve the optimal performance. In the process of optimization, the most important design parameters are grid structure, grid filling ratio and mass constraint percentage. Taking aviation rocker arm as an example, orthogonal experiment is used to get the optimal optimization parameters, which makes the lightweight effect of rocker arm better. The numerical results show that by simulating nine groups of orthogonal experiments and integrating the factors of stress, strain and weight reduction, a lattice structure is finally selected. Compared with the original model, the strain is reduced by 14%, the stress is reduced by 68% and the weight is reduced by 23%. The rocker arm is processed and manufactured by adding material manufacturing technology, which solves the weight reduction optimization problem of aviation parts rocker arm. •Topology optimization was used to the process of lattice structure design to the optimal design of variable density lattice structure.•Orthogonal experiment was used to get the optimal optimization parameters.•A new variable density lattice structure method was proposed.
doi_str_mv 10.1016/j.energy.2021.122554
format Article
fullrecord <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_journals_2638294191</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><els_id>S0360544221028036</els_id><sourcerecordid>2638294191</sourcerecordid><originalsourceid>FETCH-LOGICAL-c334t-f167443503c94e3cb1d630b400534b42c03e49170ce01513475fc8b187bd73ec3</originalsourceid><addsrcrecordid>eNp9kE1Lw0AQhhdRsFb_gYcFz4n7mY-LIOIXFHqp52WzmZQJ7abubgr115sSz54GZuZ9Z96HkHvOcs548djn4CFsT7lggudcCK3VBVnwqpRZUVb6kiyYLFimlRLX5CbGnjGmq7pekM36kHCPPzbh4GkLEbeeDh092oC22cHU8hHTie5sSuiAxhRGl8YAtBsCtW2LCY9A99aPnT0P0G9vyVVndxHu_uqSfL29bl4-stX6_fPleZU5KVXKOl6USknNpKsVSNfwtpCsUdNvUjVKOCZB1bxkDhjXXKpSd65qplhNW0pwckkeZt9DGL5HiMn0wxj8dNKIQlaiVrzm05aat1wYYgzQmUPAvQ0nw5k58zO9mfmZMz8z85tkT7MMpgRHhGCiQ_AOWgzgkmkH_N_gF_fvex4</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>2638294191</pqid></control><display><type>article</type><title>Optimization design of variable density lattice structure for additive manufacturing</title><source>Elsevier ScienceDirect Journals</source><creator>Zhang, Xinju ; Xue, Zhanpu ; Cheng, Quntao ; Ji, Yunguang</creator><creatorcontrib>Zhang, Xinju ; Xue, Zhanpu ; Cheng, Quntao ; Ji, Yunguang</creatorcontrib><description>Lattice material is a kind of super light and high strength porous material with high performance. At present, it is mainly composed of lattice structure with equal density components. In practice, each part of the lattice structure bears different loads, so the performance of the lattice structure with equal density can not be brought into full play. In view of the above problems, topology optimization was used to the process of lattice structure design to the optimal design of variable density lattice structure. According to the actual load, the optimal variable density lattice structure is designed to achieve the optimal performance. In the process of optimization, the most important design parameters are grid structure, grid filling ratio and mass constraint percentage. Taking aviation rocker arm as an example, orthogonal experiment is used to get the optimal optimization parameters, which makes the lightweight effect of rocker arm better. The numerical results show that by simulating nine groups of orthogonal experiments and integrating the factors of stress, strain and weight reduction, a lattice structure is finally selected. Compared with the original model, the strain is reduced by 14%, the stress is reduced by 68% and the weight is reduced by 23%. The rocker arm is processed and manufactured by adding material manufacturing technology, which solves the weight reduction optimization problem of aviation parts rocker arm. •Topology optimization was used to the process of lattice structure design to the optimal design of variable density lattice structure.•Orthogonal experiment was used to get the optimal optimization parameters.•A new variable density lattice structure method was proposed.</description><identifier>ISSN: 0360-5442</identifier><identifier>EISSN: 1873-6785</identifier><identifier>DOI: 10.1016/j.energy.2021.122554</identifier><language>eng</language><publisher>Oxford: Elsevier Ltd</publisher><subject>Aircraft components ; Aviation ; Density ; Design ; Design optimization ; Design parameters ; Lattice design ; Lattice structure ; Manufacturing ; Optimization ; Porous materials ; Rocker arm ; Strain ; Topology ; Topology optimization ; Variable density ; Weight reduction</subject><ispartof>Energy (Oxford), 2022-03, Vol.242, p.122554, Article 122554</ispartof><rights>2021 Elsevier Ltd</rights><rights>Copyright Elsevier BV Mar 1, 2022</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c334t-f167443503c94e3cb1d630b400534b42c03e49170ce01513475fc8b187bd73ec3</citedby><cites>FETCH-LOGICAL-c334t-f167443503c94e3cb1d630b400534b42c03e49170ce01513475fc8b187bd73ec3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktohtml>$$Uhttps://www.sciencedirect.com/science/article/pii/S0360544221028036$$EHTML$$P50$$Gelsevier$$H</linktohtml><link.rule.ids>314,776,780,3537,27901,27902,65306</link.rule.ids></links><search><creatorcontrib>Zhang, Xinju</creatorcontrib><creatorcontrib>Xue, Zhanpu</creatorcontrib><creatorcontrib>Cheng, Quntao</creatorcontrib><creatorcontrib>Ji, Yunguang</creatorcontrib><title>Optimization design of variable density lattice structure for additive manufacturing</title><title>Energy (Oxford)</title><description>Lattice material is a kind of super light and high strength porous material with high performance. At present, it is mainly composed of lattice structure with equal density components. In practice, each part of the lattice structure bears different loads, so the performance of the lattice structure with equal density can not be brought into full play. In view of the above problems, topology optimization was used to the process of lattice structure design to the optimal design of variable density lattice structure. According to the actual load, the optimal variable density lattice structure is designed to achieve the optimal performance. In the process of optimization, the most important design parameters are grid structure, grid filling ratio and mass constraint percentage. Taking aviation rocker arm as an example, orthogonal experiment is used to get the optimal optimization parameters, which makes the lightweight effect of rocker arm better. The numerical results show that by simulating nine groups of orthogonal experiments and integrating the factors of stress, strain and weight reduction, a lattice structure is finally selected. Compared with the original model, the strain is reduced by 14%, the stress is reduced by 68% and the weight is reduced by 23%. The rocker arm is processed and manufactured by adding material manufacturing technology, which solves the weight reduction optimization problem of aviation parts rocker arm. •Topology optimization was used to the process of lattice structure design to the optimal design of variable density lattice structure.•Orthogonal experiment was used to get the optimal optimization parameters.•A new variable density lattice structure method was proposed.</description><subject>Aircraft components</subject><subject>Aviation</subject><subject>Density</subject><subject>Design</subject><subject>Design optimization</subject><subject>Design parameters</subject><subject>Lattice design</subject><subject>Lattice structure</subject><subject>Manufacturing</subject><subject>Optimization</subject><subject>Porous materials</subject><subject>Rocker arm</subject><subject>Strain</subject><subject>Topology</subject><subject>Topology optimization</subject><subject>Variable density</subject><subject>Weight reduction</subject><issn>0360-5442</issn><issn>1873-6785</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2022</creationdate><recordtype>article</recordtype><recordid>eNp9kE1Lw0AQhhdRsFb_gYcFz4n7mY-LIOIXFHqp52WzmZQJ7abubgr115sSz54GZuZ9Z96HkHvOcs548djn4CFsT7lggudcCK3VBVnwqpRZUVb6kiyYLFimlRLX5CbGnjGmq7pekM36kHCPPzbh4GkLEbeeDh092oC22cHU8hHTie5sSuiAxhRGl8YAtBsCtW2LCY9A99aPnT0P0G9vyVVndxHu_uqSfL29bl4-stX6_fPleZU5KVXKOl6USknNpKsVSNfwtpCsUdNvUjVKOCZB1bxkDhjXXKpSd65qplhNW0pwckkeZt9DGL5HiMn0wxj8dNKIQlaiVrzm05aat1wYYgzQmUPAvQ0nw5k58zO9mfmZMz8z85tkT7MMpgRHhGCiQ_AOWgzgkmkH_N_gF_fvex4</recordid><startdate>20220301</startdate><enddate>20220301</enddate><creator>Zhang, Xinju</creator><creator>Xue, Zhanpu</creator><creator>Cheng, Quntao</creator><creator>Ji, Yunguang</creator><general>Elsevier Ltd</general><general>Elsevier BV</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7SP</scope><scope>7ST</scope><scope>7TB</scope><scope>8FD</scope><scope>C1K</scope><scope>F28</scope><scope>FR3</scope><scope>KR7</scope><scope>L7M</scope><scope>SOI</scope></search><sort><creationdate>20220301</creationdate><title>Optimization design of variable density lattice structure for additive manufacturing</title><author>Zhang, Xinju ; Xue, Zhanpu ; Cheng, Quntao ; Ji, Yunguang</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c334t-f167443503c94e3cb1d630b400534b42c03e49170ce01513475fc8b187bd73ec3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2022</creationdate><topic>Aircraft components</topic><topic>Aviation</topic><topic>Density</topic><topic>Design</topic><topic>Design optimization</topic><topic>Design parameters</topic><topic>Lattice design</topic><topic>Lattice structure</topic><topic>Manufacturing</topic><topic>Optimization</topic><topic>Porous materials</topic><topic>Rocker arm</topic><topic>Strain</topic><topic>Topology</topic><topic>Topology optimization</topic><topic>Variable density</topic><topic>Weight reduction</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Zhang, Xinju</creatorcontrib><creatorcontrib>Xue, Zhanpu</creatorcontrib><creatorcontrib>Cheng, Quntao</creatorcontrib><creatorcontrib>Ji, Yunguang</creatorcontrib><collection>CrossRef</collection><collection>Electronics &amp; Communications Abstracts</collection><collection>Environment Abstracts</collection><collection>Mechanical &amp; Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Environmental Sciences and Pollution Management</collection><collection>ANTE: Abstracts in New Technology &amp; Engineering</collection><collection>Engineering Research Database</collection><collection>Civil Engineering Abstracts</collection><collection>Advanced Technologies Database with Aerospace</collection><collection>Environment Abstracts</collection><jtitle>Energy (Oxford)</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Zhang, Xinju</au><au>Xue, Zhanpu</au><au>Cheng, Quntao</au><au>Ji, Yunguang</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Optimization design of variable density lattice structure for additive manufacturing</atitle><jtitle>Energy (Oxford)</jtitle><date>2022-03-01</date><risdate>2022</risdate><volume>242</volume><spage>122554</spage><pages>122554-</pages><artnum>122554</artnum><issn>0360-5442</issn><eissn>1873-6785</eissn><abstract>Lattice material is a kind of super light and high strength porous material with high performance. At present, it is mainly composed of lattice structure with equal density components. In practice, each part of the lattice structure bears different loads, so the performance of the lattice structure with equal density can not be brought into full play. In view of the above problems, topology optimization was used to the process of lattice structure design to the optimal design of variable density lattice structure. According to the actual load, the optimal variable density lattice structure is designed to achieve the optimal performance. In the process of optimization, the most important design parameters are grid structure, grid filling ratio and mass constraint percentage. Taking aviation rocker arm as an example, orthogonal experiment is used to get the optimal optimization parameters, which makes the lightweight effect of rocker arm better. The numerical results show that by simulating nine groups of orthogonal experiments and integrating the factors of stress, strain and weight reduction, a lattice structure is finally selected. Compared with the original model, the strain is reduced by 14%, the stress is reduced by 68% and the weight is reduced by 23%. The rocker arm is processed and manufactured by adding material manufacturing technology, which solves the weight reduction optimization problem of aviation parts rocker arm. •Topology optimization was used to the process of lattice structure design to the optimal design of variable density lattice structure.•Orthogonal experiment was used to get the optimal optimization parameters.•A new variable density lattice structure method was proposed.</abstract><cop>Oxford</cop><pub>Elsevier Ltd</pub><doi>10.1016/j.energy.2021.122554</doi></addata></record>
fulltext fulltext
identifier ISSN: 0360-5442
ispartof Energy (Oxford), 2022-03, Vol.242, p.122554, Article 122554
issn 0360-5442
1873-6785
language eng
recordid cdi_proquest_journals_2638294191
source Elsevier ScienceDirect Journals
subjects Aircraft components
Aviation
Density
Design
Design optimization
Design parameters
Lattice design
Lattice structure
Manufacturing
Optimization
Porous materials
Rocker arm
Strain
Topology
Topology optimization
Variable density
Weight reduction
title Optimization design of variable density lattice structure for additive manufacturing
url https://sfx.bib-bvb.de/sfx_tum?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-02-04T06%3A49%3A40IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Optimization%20design%20of%20variable%20density%20lattice%20structure%20for%20additive%20manufacturing&rft.jtitle=Energy%20(Oxford)&rft.au=Zhang,%20Xinju&rft.date=2022-03-01&rft.volume=242&rft.spage=122554&rft.pages=122554-&rft.artnum=122554&rft.issn=0360-5442&rft.eissn=1873-6785&rft_id=info:doi/10.1016/j.energy.2021.122554&rft_dat=%3Cproquest_cross%3E2638294191%3C/proquest_cross%3E%3Curl%3E%3C/url%3E&disable_directlink=true&sfx.directlink=off&sfx.report_link=0&rft_id=info:oai/&rft_pqid=2638294191&rft_id=info:pmid/&rft_els_id=S0360544221028036&rfr_iscdi=true