Multi-objective topology optimization of aero-engine accessory gearbox case based on compromise programming method

The accessory gearbox is a crucial component of the power transmission system of an aero-engine. The current design of the accessory gearbox case heavily relies on engineering experience, resulting in a bulky and heavy structure. This makes it increasingly challenging to meet the design requirements...

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Veröffentlicht in:Science China. Technological sciences Jg. 68; H. 7; S. 1720601
Hauptverfasser: Huang, Hao, Wang, Zeng, Yang, Ziyi, Liu, Huaiju, Lu, Zehua
Format: Journal Article
Sprache:Englisch
Veröffentlicht: Beijing Science China Press 01.07.2025
Springer Nature B.V
Schlagworte:
ISSN:1674-7321, 1869-1900
Online-Zugang:Volltext
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Zusammenfassung:The accessory gearbox is a crucial component of the power transmission system of an aero-engine. The current design of the accessory gearbox case heavily relies on engineering experience, resulting in a bulky and heavy structure. This makes it increasingly challenging to meet the design requirements of high-power density. This work proposes a multi-objective topology optimization method based on the compromise programming method for the aero-engine accessory gearbox case. By locally thinning the gearbox case wall thickness, the case weight is reduced by 12.7%, and the maximum Mises stress is also reduced by 19.7% compared to the initial design scheme. Furthermore, the maximum vibration acceleration amplitude is reduced by 23.9%. These results provide a new solution for the lightweight design of the aero-engine accessory gearbox case.
Bibliographie:ObjectType-Article-1
SourceType-Scholarly Journals-1
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content type line 14
ISSN:1674-7321
1869-1900
DOI:10.1007/s11431-024-2915-3