首页|A discussion of fatigue properties of notched specimens subjected to prestressing treatment machined from FGH4097

A discussion of fatigue properties of notched specimens subjected to prestressing treatment machined from FGH4097

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Experimental and numerical investigations were performed to reveal the effect of pre-stress on the fatigue properties of FGH4097 so as to quantitatively evaluate the overspeed benefit of the disc of aeroengine.A corresponding experiment was performed to examine the effect of pre-stress on the fatigue life of FGH97.A complete model describing the fatigue properties of the pre-stressed notch specimen was proposed.After the modification of mean stress,stress gradient and prestressing treatment,the model is finally verified by fatigue test of presstressed notch specimens machined from FGH4097 with satisfactory accuracy and good engineering applicability.The new model highlights that for the variable fatigue loads,the introduction of appropriate prestress is expected to benefit to the notch specimens and certainly to the disc of aeroengine regards of their fatigue properties.Both the calculation method of fatigue life parameters and the prestress correc-tion model are proved to have good prediction accuracy.

Turbine bliskOverspeed testPrestressFatigue life predictionFGH4097

Rongxi SHI、Dasheng WEI、Le HAN、Shun YANG

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School of Energy and Power Engineering,Beihang University,Beijing 100191,China

Jiangxi Research Institute,Beihang University,Nanchang 330096,China

Research Institute of Aero-Engine,Beihang University,Beijing 100191,China

国家科技重大专项国家自然科学基金中国博士后科学基金

J2019-IV-0012-0080122020302022M720340

2024

中国航空学报(英文版)
中国航空学会

中国航空学报(英文版)

CSTPCDEI
影响因子:0.847
ISSN:1000-9361
年,卷(期):2024.37(4)
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