Creep Data Prediction for Aluminium Airframe Alloys

机译：铝机身合金的蠕变数据预测

获取原文

获取原文并翻译 | 示例

页面导航

摘要
著录项
相似文献
相关主题

摘要

Constant-stress creep tests have been completed for 2124-T851 at stresses giving creep lives up to 1,000 hours at 423 and 463K. The results were analysed using the θ Projection Concept, which quantifies the variations in creep curve shape with stress and temperature, allowing accurate prediction of stress rupture data for times up to 100,000 hours at 423K.

机译：2124-T851的恒应力蠕变测试已经完成，其应力可在423和463K时提供长达1000小时的蠕变寿命。使用θ投影概念对结果进行了分析，该概念可量化蠕变曲线形状随应力和温度的变化，从而可以在423K时准确预测长达100,000小时的应力破裂数据。

著录项

来源
《International Conference on Processing amp; Manufacturing of Advanced Materials Pt.1; Jul 7-11, 2003; Leganes, Madrid, Spain》|2003年|p.261-266|共6页
会议地点 Madrid(ES);Madrid(ES)
作者
B. Wilshire; H. Burt;
展开▼
作者单位

Materials Research Centre, School of Engineering, University of Wales Swansea, Singleton Park, Swansea SA2 8PP, United Kingdom;

展开▼
会议组织
原文格式 PDF
正文语种 eng
中图分类一般工业技术;
关键词
2124-T851; creep; creep fracture; creep data extrapolation.;

机译：2124-T851;蠕变;蠕变断裂;蠕变数据外推。;

相似文献

外文文献
中文文献
专利

1. Rationalization of Short-Term Creep Test Data and Prediction of Long-Term Creep Strengths of a Fe-20Cr-25Ni (WtPct) Austenitic Stainless Steel (Alloy 709) [J] . Yi P. C., Jiang C. C., Dong Z., Metallurgical and Materials Transactions, A. Physical Metallurgy and Materials Science . 2019,第8期

机译：短期蠕变试验数据的合理化和Fe-20cr-25ni（WTPCT）奥氏体不锈钢长期蠕变强度的预测（合金709）
2. Long-term creep strength predictions from short-term creep test data for high Cr creep-resistant steels and microstructural evolution origin of over-predictions [J] . Gao J., Yi P. C., Song X. L., Materials at High Temperatures . 2019,第4期

机译：短期蠕变强度预测从短期蠕变测试数据进行高CR蠕变钢和过度预测的微观结构演变起源
3. Constitutive modelling and springback prediction for creep age forming of 2124 aluminium alloy [J] . X. L Xu, L H. Zhan, Y. G. Li Materials Science and Technology: MST: A publication of the Institute of Metals . 2013,第9期

机译：2124铝合金蠕变时效的本构建模与回弹预测。
4. Creep Data Prediction for Aluminium Airframe Alloys [C] . B. Wilshire, H. Burt International Conference on Processing and Manufacturing of Advanced Materials . 2003

机译：铝机身合金的蠕变数据预测
5. Effect of Alloying Additions of Aluminium and Iron on the Creep Resistance of Ti-12Cr (Wt.%) [D] . Chakravarty, Harish Narasimhan. 2019

机译：合金加入铝和铁的影响Ti-12Cr（wt.％）的蠕变抗性
6. Data set on prediction of friction stir welding parameters to achieve maximum strength of AA2014-T6 aluminium alloy joints [O] . C. Rajendran, K. Srinivasan, V. Balasubramanian, 2019

机译：达到最大强度AA2014-T6铝合金接头的搅拌摩擦焊接参数预测数据集
7. Development of an improved model for predicting fatigue crack growth in aluminium alloy helicopter airframe components [O] . Bos M.J. 2007

机译：改进的铝合金直升机机身部件疲劳裂纹扩展预测模型的开发
8. Introduction to a Library of Creep and Strain Recovery Data for DTD 5070A Aluminium Alloy. [R] . Webb, J. N. 1977

机译：DTD 5070a铝合金蠕变和应变恢复数据库简介。

Creep Data Prediction for Aluminium Airframe Alloys

摘要

著录项

相似文献

相关主题

期刊订阅