SHEN Xiang1, CAO Peng2.Contact State Analysis of Turboshaft Engine Rotor with Curvic-Coupling Joint Structure[J].航空发动机,2017,43(4):35-40
Contact State Analysis of Turboshaft Engine Rotor with Curvic-Coupling Joint Structure
DOI:
Key Words:curvic-coupling  contact form  contact
Author NameAffiliationE-mail
SHEN Xiang1, CAO Peng2 1. COMAC Shanghai Aircraft Design and Research Institute, Shanghai 201210, China
2. AECC China Aviation Powerplant Research Institute, Zhuzhou Hunan 412002, China 
shenxiang@comac.cc 
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Abstract:In order to study the mechanismand law of contact state change of curvic-coupling of turboshaft engine rotor, the influencing factors of contact state for curvic -coupling joint structure were determined according to the structure characteristics, mechanics characteristics, and force principle of tangential contact considering sliding, and the changing rule of contact state for curvic-coupling was studied by finite element analysis method. The calculating results indicate that revolving speed and axial preload have important effects on curvic-coupling contact state; the greater the revolving speed is, the smaller the contact area is, and the greater the contact stress and sliding distance are; the greater the axis preload is, the greater the contact area is, and the greater the contact stress and sliding distance are; and the influence of friction coefficient on contact state is not obvious. The study results provide technical guidance of structure design for rotor with curvic-coupling.
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