热塑性复合材料速率增强刚性表皮：案例研究

IF 0.2 4区材料科学 Q4 ENGINEERING, MULTIDISCIPLINARY

SAMPE Journal Pub Date : 2023-11-01 DOI:10.33599/sj.v59no6.01

Joseph P. Heil, Mark A. Wadsworth, K. Dando, Ron E. Jones, Matt Tymes, Sam J Slater, Rodney E. Bahr, Bryan T. Bearden

{"title":"热塑性复合材料速率增强刚性表皮：案例研究","authors":"Joseph P. Heil, Mark A. Wadsworth, K. Dando, Ron E. Jones, Matt Tymes, Sam J Slater, Rodney E. Bahr, Bryan T. Bearden","doi":"10.33599/sj.v59no6.01","DOIUrl":null,"url":null,"abstract":"Spirit AeroSystems is developing a thermoplastic technology demonstrator featuring an out of autoclave fabrication approach. Furthermore, the intent is to demonstrate the capability in the United States and preferably at our own domestic facility. The chosen configuration is a fuselage skin panel about 1.2 m wide and 2.2 m long with five stringers and four frames. Laser assisted thermoplastic Automated Fiber Placement (AFP) is used to manufacture the skin; stringers are stamp formed, and frames used two fabrication paths: stamp forming and oven consolidation. Co-Fusion simultaneously consolidates the skin and welds stringers to the skin followed by a separate frame welding process.","PeriodicalId":49577,"journal":{"name":"SAMPE Journal","volume":null,"pages":null},"PeriodicalIF":0.2000,"publicationDate":"2023-11-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Thermoplastic Composite Rate Enhanced Stiffened Skin: A Case Study\",\"authors\":\"Joseph P. Heil, Mark A. Wadsworth, K. Dando, Ron E. Jones, Matt Tymes, Sam J Slater, Rodney E. Bahr, Bryan T. Bearden\",\"doi\":\"10.33599/sj.v59no6.01\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"Spirit AeroSystems is developing a thermoplastic technology demonstrator featuring an out of autoclave fabrication approach. Furthermore, the intent is to demonstrate the capability in the United States and preferably at our own domestic facility. The chosen configuration is a fuselage skin panel about 1.2 m wide and 2.2 m long with five stringers and four frames. Laser assisted thermoplastic Automated Fiber Placement (AFP) is used to manufacture the skin; stringers are stamp formed, and frames used two fabrication paths: stamp forming and oven consolidation. Co-Fusion simultaneously consolidates the skin and welds stringers to the skin followed by a separate frame welding process.\",\"PeriodicalId\":49577,\"journal\":{\"name\":\"SAMPE Journal\",\"volume\":null,\"pages\":null},\"PeriodicalIF\":0.2000,\"publicationDate\":\"2023-11-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"SAMPE Journal\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://doi.org/10.33599/sj.v59no6.01\",\"RegionNum\":4,\"RegionCategory\":\"材料科学\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q4\",\"JCRName\":\"ENGINEERING, MULTIDISCIPLINARY\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"SAMPE Journal","FirstCategoryId":"5","ListUrlMain":"https://doi.org/10.33599/sj.v59no6.01","RegionNum":4,"RegionCategory":"材料科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q4","JCRName":"ENGINEERING, MULTIDISCIPLINARY","Score":null,"Total":0}

引用次数: 0

摘要

Spirit AeroSystems 公司正在开发一种热塑性塑料技术演示器，其特点是采用高压釜外制造方法。此外，我们还打算在美国，最好是在我们自己的国内工厂演示这种能力。我们选择的配置是宽约 1.2 米、长约 2.2 米的机身蒙皮面板，包括五根弦杆和四个框架。蒙皮采用激光辅助热塑性塑料自动纤维贴装技术（AFP）制造；弦杆采用冲压成型，框架采用两种制造路径：冲压成型和烘箱固结。共熔同时对表皮进行加固，并将弦杆焊接到表皮上，然后再进行单独的框架焊接工艺。

本文章由计算机程序翻译，如有差异，请以英文原文为准。

查看原文本刊更多论文

Thermoplastic Composite Rate Enhanced Stiffened Skin: A Case Study

Spirit AeroSystems is developing a thermoplastic technology demonstrator featuring an out of autoclave fabrication approach. Furthermore, the intent is to demonstrate the capability in the United States and preferably at our own domestic facility. The chosen configuration is a fuselage skin panel about 1.2 m wide and 2.2 m long with five stringers and four frames. Laser assisted thermoplastic Automated Fiber Placement (AFP) is used to manufacture the skin; stringers are stamp formed, and frames used two fabrication paths: stamp forming and oven consolidation. Co-Fusion simultaneously consolidates the skin and welds stringers to the skin followed by a separate frame welding process.

求助全文

通过发布文献求助，成功后即可免费获取论文全文。去求助

来源期刊

SAMPE Journal 工程技术-材料科学：综合

CiteScore

0.16

自引率

0.00%

发文量

审稿时长

>12 weeks

期刊介绍： SAMPE Journal readers represent the diversity of the advanced materials and processes industry. Our readers are creative and innovative, they publish, they develop concepts, they win patents, they move the world of materials and processes. Join thought leaders – academicians, engineers, scientists, business leaders, researchers, suppliers, manufacturers – and become a reader of the industry’s only technical journal dedicated to advanced materials and processes.