Microstructural deterioration mechanism of directionally solidified Ni-based superalloy used in first-stage industrial gas turbine blades after ultra long-term service-Reference-Cited by-同舟云学术

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Microstructural deterioration mechanism of directionally solidified Ni-based superalloy used in first-stage industrial gas turbine blades after ultra long-term service

Published:2024-07 Issue: Volume:213 Page:114000
ISSN:1044-5803
Container-title:Materials Characterization
language:en
Short-container-title:Materials Characterization

Author:

Chen Yang,Yao Zhihao,Dong Jianxin,Yang Huanyu,Ren Mo,Peng Jialin,Leng Liuxi,Zhang Xiaoming,Yang Jingming

Publisher

Elsevier BV

Reference57 articles.

1. Design and control challenges of hybrid, dual nozzle gas turbine power generating plant: a critical review;Kulor;Energy Rep.,2021

2. Improvement of gas turbine performance based on inlet air cooling systems: a technical review;Ibrahim;Int. J. Phys. Sci.,2011

3. Efficiency of chemically recuperated gas turbine fired with methane: effect of operating parameters;Pashchenko;Appl. Therm. Eng.,2022

4. A review on the corrosion and fatigue failure of gas turbines;Fathyunes;Metals,2023

5. Meso-scale low-cycle fatigue damage of polycrystalline nickel-based alloy by crystal plasticity finite element method;Long;Int. J. Fatigue,2023

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Microstructural evolution and diffusion mechanism of MCrAlY coated nickel-based superalloy turbine blades after serviced for 47,000 h;Surface and Coatings Technology;2024-10

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