胡绪腾

Associate Professor   Supervisor of Master's Candidates

Gender:Male

Alma Mater:南京航空航天大学

Education Level:南京航空航天大学

Degree:Doctoral Degree in Engineering

School/Department:College of Energy and Power Engineering

Discipline:能源动力. Power Machinery and Engineering. Aerospace Propulsion Theory and Engineering

Contact Information:13814089286

E-Mail:


Paper Publications

Effect of notch geometry on the fatigue strength and critical distance of TC4 titanium alloy

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Affiliation of Author(s):能源与动力学院

Journal:JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY

Key Words:HCF strength Notch geometry TC4 Stress concentration Critical distance size effect

Abstract:Studying the effect of different geometric features of machined notch on the fatigue strength and critical distance has an important guiding role to understand the critical distance size effect and to predict the HCF strength of turbine engine fan blades after FOD. Systematically experimental investigations of geometrical characteristic effects on the 106 cycle fatigue strength and critical distance for TC4 machined notched plates at stress ratios of R = 0.1 have been conducted. 123 specimens, including unnotched plates and three different types of notched plates (V-notches, U-notches and C-notches) with various notch root radii, depths and angles have been considered. The results indicate that the notch with small radius can significantly lead to high stress concentration and greatly reduce the HCF strength, while the notch angle and notch depth can affect the HCF strength to a certain extent. The Kt related model does not apply to describe the critical distance size effect perfectly. The critical distance has linear relationship with the notch root radius but no significant correction with the notch depth or notch angle. The findings of this study are beneficial for the size effect modeling and later fatigue strength evaluating of TC4 notched components.

ISSN No.:1738-494X

Translation or Not:no

Date of Publication:2017-10-01

Co-author:djx,Bao, Zhenqiang,syd

Correspondence Author:syd,Hu Xuteng

Pre One:镍基高温合金紧凑拉伸试样侧槽优选研究及试验

Next One:Fatigue Hysteresis Behavior of 2.5D Woven C/SiC Composites: Theory and Experiments

Profile

1998年9月~2009年9月本科、硕士和博士均就读于南京航空航天大学能源与动力学院航空发动机专业。2009年10月至今就职于南京航空航天大学能源与动力学院,现担任中国航空发动机集团科技委结构强度与振动专业委员会委员。主要从事发动机结构完整性和耐久性方面的教学和科研工作,研究兴趣包括:发动机结构静强度分析与设计技术,发动机结构疲劳寿命预测技术,发动机结构损伤容限设计与试验技术,发动机结构蠕变分析与持久寿命预测技术,发动机寿命监视与寿命管理技术,发动机结构方案设计技术。先后主持军科委基础加强项目课题、“两机专项”基础研究项目专题、国家自然科学基金、航空科学基金、国防预研等科研课题10余项。荣获省部级科技成果三等奖1项(排名第三),发表学术论文60余篇(其中SCI/EI检索论文30余篇)。