首页|Optimizing circumferential assembly angle of rotor parts connected by curvic couplings based on acquired tooth surface error data

Optimizing circumferential assembly angle of rotor parts connected by curvic couplings based on acquired tooth surface error data

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Due to the excellent self-centering and load-carrying capability,curvic couplings have been widely used in advanced aero-engine rotors.However,curvic tooth surface errors lead to poor assembly precision.Traditional physical-master-gauge-based indirect tooth surface error measure-ment and circumferential assembly angle optimization methods have the disadvantages of high cost and weak generality.The unknown tooth surface fitting mechanism is a big barrier to assembly pre-cision prediction and improvement.Therefore,this work puts forward a data-driven assembly sim-ulation and optimization approach for aero-engine rotors connected by curvic couplings.The origin of curvic tooth surface error is deeply investigated.Using 5-axis sweep scan method,a large amount of high-precision curvic tooth surface data are acquired efficiently.Based on geometric models of parts,the fitting mechanism of curvic couplings is uncovered for assembly precision simulation and prediction.A circumferential assembly angle optimization model is developed to decrease axial and radial assembly runouts.Experimental results show that the assembly precision can be pre-dicted accurately and improved dramatically.By uncovering the essential principle of the assembly precision formation and proposing circumferential assembly angle optimization model,this work is meaningful for assembly quality,efficiency and economy improvement of multistage aero-engine rotors connected by curvic couplings.

Curvic couplingsTooth surface errorAssembly precisionAxial and radial runoutsCircumferential assembly angle

Huibin SUN、Meng LIUa、Yingzhi ZHANG、Chenle WEI

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Key Laboratory of High Performance Manufacturing for Aero Engine,Ministry of Industry and Information Technology,Northwestern Polytechnical University,Xi'an 710072,China

AECC South Industry Company Limited,Zhuzhou 412002,China

National Basic Research ProjectNational Basic Research Project中央高校基本科研业务费专项国家自然科学基金

J2022-Ⅶ-0001-00432017-Ⅶ-0010-010472231008

2024

10.1016/j.cja.2023.11.019

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(3)
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