ATI 718Plus的蠕变断裂性能——一种稀疏数据评估方法

IF 1 4区 材料科学 Q4 MATERIALS SCIENCE, MULTIDISCIPLINARY Materials at High Temperatures Pub Date : 2022-10-31 DOI:10.1080/09603409.2022.2135721
C. Bullough, E. Debruycker, E. Poggio, M. Schwienheer, M. Spindler
{"title":"ATI 718Plus的蠕变断裂性能——一种稀疏数据评估方法","authors":"C. Bullough, E. Debruycker, E. Poggio, M. Schwienheer, M. Spindler","doi":"10.1080/09603409.2022.2135721","DOIUrl":null,"url":null,"abstract":"ABSTRACT The nickel-base alloy ATI 718Plus © (UNS N07818) was introduced in 2003 with the intention of providing similar properties to Waspaloy but having the fabricability of Alloy 718. Such characteristics make it of strong interest for use in aeroengines for disk forgings, blades and bolting bar. Within power generation, the advent of higher temperatures in industrial gas turbines, and advanced supercritical steam turbines, the combination of properties and processability make it an increasingly attractive proposition for a range of applications. This paper reports an exploratory creep test programme of beyond 30 kh duration leading to an Interim ECCC Datasheet on ATI 718Plus. It demonstrates how even small volumes of test data can be assessed to produce a datasheet that can be used for preliminary design. In particular, it considers how best to determine the rupture behaviour, by including the data from unfailed tests, using both polynomial and Wilshire Equation models, with coefficients estimated by conventional regression estimation, and also with maximum likelihood methods. Additionally, creep-strain time data are modelled and extrapolated, using simplified equations developed and/or applied within the ECCC in recent work. The results confirm the temperature advantage in creep of 718Plus over Alloy 718. Recommendations of how to assess sparse datasets have also resulted from this work, leading to an expectation that new materials can be developed more quickly and with higher reliability. Nevertheless, there is no substitute for long-term multi-heat testing to prove the predicted behaviour and to examine the stability of materials in the long term.","PeriodicalId":49877,"journal":{"name":"Materials at High Temperatures","volume":"1 1","pages":"655 - 667"},"PeriodicalIF":1.0000,"publicationDate":"2022-10-31","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"1","resultStr":"{\"title\":\"Creep rupture properties of ATI 718Plus – an approach to assessing sparse data\",\"authors\":\"C. Bullough, E. Debruycker, E. Poggio, M. Schwienheer, M. Spindler\",\"doi\":\"10.1080/09603409.2022.2135721\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"ABSTRACT The nickel-base alloy ATI 718Plus © (UNS N07818) was introduced in 2003 with the intention of providing similar properties to Waspaloy but having the fabricability of Alloy 718. Such characteristics make it of strong interest for use in aeroengines for disk forgings, blades and bolting bar. Within power generation, the advent of higher temperatures in industrial gas turbines, and advanced supercritical steam turbines, the combination of properties and processability make it an increasingly attractive proposition for a range of applications. This paper reports an exploratory creep test programme of beyond 30 kh duration leading to an Interim ECCC Datasheet on ATI 718Plus. It demonstrates how even small volumes of test data can be assessed to produce a datasheet that can be used for preliminary design. In particular, it considers how best to determine the rupture behaviour, by including the data from unfailed tests, using both polynomial and Wilshire Equation models, with coefficients estimated by conventional regression estimation, and also with maximum likelihood methods. Additionally, creep-strain time data are modelled and extrapolated, using simplified equations developed and/or applied within the ECCC in recent work. The results confirm the temperature advantage in creep of 718Plus over Alloy 718. Recommendations of how to assess sparse datasets have also resulted from this work, leading to an expectation that new materials can be developed more quickly and with higher reliability. Nevertheless, there is no substitute for long-term multi-heat testing to prove the predicted behaviour and to examine the stability of materials in the long term.\",\"PeriodicalId\":49877,\"journal\":{\"name\":\"Materials at High Temperatures\",\"volume\":\"1 1\",\"pages\":\"655 - 667\"},\"PeriodicalIF\":1.0000,\"publicationDate\":\"2022-10-31\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"1\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Materials at High Temperatures\",\"FirstCategoryId\":\"88\",\"ListUrlMain\":\"https://doi.org/10.1080/09603409.2022.2135721\",\"RegionNum\":4,\"RegionCategory\":\"材料科学\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q4\",\"JCRName\":\"MATERIALS SCIENCE, MULTIDISCIPLINARY\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Materials at High Temperatures","FirstCategoryId":"88","ListUrlMain":"https://doi.org/10.1080/09603409.2022.2135721","RegionNum":4,"RegionCategory":"材料科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q4","JCRName":"MATERIALS SCIENCE, MULTIDISCIPLINARY","Score":null,"Total":0}
引用次数: 1

摘要

镍基合金ATI 718Plus©(UNS N07818)于2003年推出,旨在提供与沃斯帕洛伊合金相似的性能,但具有718合金的可制造性。这些特性使其在航空发动机的圆盘锻件、叶片和螺栓杆中具有浓厚的兴趣。在发电领域,高温工业燃气轮机的出现,以及先进的超临界汽轮机,其性能和可加工性的结合使其在一系列应用中越来越有吸引力。本文报告了一个探索性蠕变测试程序,超过30kh持续时间,导致ATI 718Plus上的临时ECCC数据表。它演示了如何评估少量的测试数据以产生可用于初步设计的数据表。特别是,它考虑了如何最好地确定破裂行为,通过使用多项式和Wilshire方程模型,使用传统回归估计估计的系数,以及最大似然方法,包括来自未失败试验的数据。此外,蠕变应变时间数据建模和外推,使用简化方程开发和/或在ECCC最近的工作中应用。结果证实了718Plus在蠕变方面比718合金具有温度优势。关于如何评估稀疏数据集的建议也来自这项工作,导致人们期望新材料可以更快地开发,具有更高的可靠性。然而,没有什么可以替代长期的多热测试来证明预测的行为,并检查材料的长期稳定性。
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
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
Creep rupture properties of ATI 718Plus – an approach to assessing sparse data
ABSTRACT The nickel-base alloy ATI 718Plus © (UNS N07818) was introduced in 2003 with the intention of providing similar properties to Waspaloy but having the fabricability of Alloy 718. Such characteristics make it of strong interest for use in aeroengines for disk forgings, blades and bolting bar. Within power generation, the advent of higher temperatures in industrial gas turbines, and advanced supercritical steam turbines, the combination of properties and processability make it an increasingly attractive proposition for a range of applications. This paper reports an exploratory creep test programme of beyond 30 kh duration leading to an Interim ECCC Datasheet on ATI 718Plus. It demonstrates how even small volumes of test data can be assessed to produce a datasheet that can be used for preliminary design. In particular, it considers how best to determine the rupture behaviour, by including the data from unfailed tests, using both polynomial and Wilshire Equation models, with coefficients estimated by conventional regression estimation, and also with maximum likelihood methods. Additionally, creep-strain time data are modelled and extrapolated, using simplified equations developed and/or applied within the ECCC in recent work. The results confirm the temperature advantage in creep of 718Plus over Alloy 718. Recommendations of how to assess sparse datasets have also resulted from this work, leading to an expectation that new materials can be developed more quickly and with higher reliability. Nevertheless, there is no substitute for long-term multi-heat testing to prove the predicted behaviour and to examine the stability of materials in the long term.
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
Materials at High Temperatures
Materials at High Temperatures 工程技术-材料科学:综合
CiteScore
1.90
自引率
15.40%
发文量
58
审稿时长
>12 weeks
期刊介绍: Materials at High Temperatures welcomes contributions relating to high temperature applications in the energy generation, aerospace, chemical and process industries. The effects of high temperatures and extreme environments on the corrosion and oxidation, fatigue, creep, strength and wear of metallic alloys, ceramics, intermetallics, and refractory and composite materials relative to these industries are covered. Papers on the modelling of behaviour and life prediction are also welcome, provided these are validated by experimental data and explicitly linked to actual or potential applications. Contributions addressing the needs of designers and engineers (e.g. standards and codes of practice) relative to the areas of interest of this journal also fall within the scope. The term ''high temperatures'' refers to the subsequent temperatures of application and not, for example, to those of processing itself. Materials at High Temperatures publishes regular thematic issues on topics of current interest. Proposals for issues are welcomed; please contact one of the Editors with details.
期刊最新文献
Effect of concave–convex degree of substrate surface on thermal shock performance of Cr coating Estimating the Monkman−Grant relation in the presence of errors in measurement of times to failure and minimum creep rates: with application to some high temperature materials Comparative assessment of a continuum damage mechanics-based creep damage models for India-specific RAFM steel A comparison of hyperbolic sine creep life equations and data correlation methods for these equations Microstructure evolution of Incoloy 800H in industrial environment and correlation with creep mechanisms from literature
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1