详细信息

A prediction model of erosion rate under erosion-tension coupling for engine blade  ( SCI-EXPANDED收录 EI收录)  

文献类型:期刊文献

英文题名:A prediction model of erosion rate under erosion-tension coupling for engine blade

作者:Zhang, Yu[1];Jia, Yun-Fei[1];Sun, Xin-Wei[1];Fang, Zhen-Hua[1];Yan, Jian-Jun[1];Zhang, Cheng-Cheng[2];Xin, Li[3];Zhang, Xian-Cheng[1]

机构:[1]East China Univ Sci & Technol, Sch Mech & Power Engn, Key Lab Pressure Syst & Safety, Minist Educ, Shanghai 200237, Peoples R China;[2]AECC Commercial Aircraft Engine Co LTD, Shanghai Engn Res Ctr Commercial Aircraft Engine, Shanghai 201108, Peoples R China;[3]Chinese Acad Sci, Inst Met Res, Shi Changxu Innovat Ctr Adv Mat, 62 Wencui Rd, Shenyang 110016, Peoples R China

年份:2025

卷号:560

外文期刊名:WEAR

收录:;EI(收录号:20244517320326);WOS:【SCI-EXPANDED(收录号:WOS:001352905200001)】;

基金:This work was sponsored by the National Natural Science Founda-tion of China (52222505 and 52321002) and Natural Science Founda-tion of Shanghai (23ZR1415500) .

语种:英文

外文关键词:Erosion model; Erosion-tension coupling; Engine blade; Erosion rate prediction; Fluid-structure interaction

摘要:The influence of solid particle erosion on aero-engine performance poses a potential threat to aviation safety. Accurate prediction of erosion rates for blades is crucial for assessing the engine's operational lifespan. Engine blades experience centrifugal forces during operation, resulting in erosion under tensile stress. This study has designed a specialized erosion-tension coupling test apparatus to explore the effect of tensile stress on specimens subjected to gas-solid erosion. Applying an axial tensile load equivalent to 60 % of the yield strength prompts a 90.2 % increase in erosion rate for aluminum alloy specimens at a 60 degrees erosion angle. Additionally, fluid-structure interaction simulations systematically analyze the surface stress distribution of specimens under various erosion and tension conditions. Subsequently, a novel erosion model is proposed, incorporating an innovative acceleration factor that considers material yield strength, Von Mises stress distribution, and erosion crater volume. This developed model accurately predicts erosion rates under various loading conditions for cylindrical and simplified engine blade specimens, with a deviation from experimental erosion rates of less than 18.1 %. The constructed erosion model provides a concise and accurate prediction of erosion rates for specimens subjected to gas-solid erosion under tensile stress.

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