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- W2391030829 abstract "In order to improve the stress state of the aero engine fan disc,and reduce its weight,in this paper,the fan disc was simplified to two-dimensional axisymmetric model and the random search methods were used under ANSYS software to optimize the fan disc structure size.Then,the three dimensional fan disc models of the original disc and optimum disc were built under the working condition,and the contact analyses were simulated Simultaneously.The weight of the fan disc has been reduced as the main structure size changed.By comprising the structural analysis results of the design state and optimizing state,we find that the stress distribution gradient of the blade/disc combination model and single disc model is reduced significantly,and the stress value is decreased in some degree.The weight of disc is reduced are improved." @default.
- W2391030829 created "2016-06-24" @default.
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- W2391030829 date "2013-01-01" @default.
- W2391030829 modified "2023-09-24" @default.
- W2391030829 title "Structure Optimum Design of Arc Tenon Fan Disc" @default.
- W2391030829 hasPublicationYear "2013" @default.
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