Progress in additive manufacturing, additive repair and fatigue evaluation of aviation titanium alloy blades-Reference-Cited by-同舟云学术

Progress in additive manufacturing, additive repair and fatigue evaluation of aviation titanium alloy blades

Published:2023-11-02 Issue:12 Volume:11 Page:973-1012
ISSN:2166-3831
Container-title:Materials Research Letters
language:en
Short-container-title:Materials Research Letters

Author:

Wang Lingfeng¹,Li Yinghong¹,Zhou Liucheng¹,Lou Yanshan²,Liu Shijie³,Zheng Dayong³,Yi Min⁴^ORCID

Affiliation:

1. National Key Lab of Aerospace Power System and Plasma Technology, Air Force Engineering University, Xi’an, People’s Republic of China

2. School of Mechanical Engineering, Xi’an Jiao Tong University, Xi’an, People’s Republic of China

3. Beijing Aerospace Propulsion Institute & Laboratory of Science and Technology on Cryogenic Liquid Propulsion, Beijing, People’s Republic of China

4. State Key Laboratory of Mechanics and Control for Aerospace Structures & Institute for Frontier Science & College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, People’s Republic of China

Funder

National Major Science and Technology Project of China

National Natural Science Foundation of China

Publisher

Informa UK Limited

Subject

General Materials Science

Link

https://www.tandfonline.com/doi/pdf/10.1080/21663831.2023.2275599

Reference234 articles.

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3. MIL-HDBK-1783B US Department of Defense; 2002.

4. GJB 241A-2010. General specification for aero turbojet and turbofan engines. Beijing: Equipment Development Department of the Central Military Commission; 2010. (in Chinese)

5. Garrison B. High cycle fatigue (HCF) science and technology program 2000 annual report; 2001.