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连续纤维增强金属基复合材料涡轮轴结构承扭特性分析
引用本文:沙云东,贾秋月,骆丽,赵奉同,栾孝驰.连续纤维增强金属基复合材料涡轮轴结构承扭特性分析[J].航空动力学报,2016,31(6):1377-1384.
作者姓名:沙云东  贾秋月  骆丽  赵奉同  栾孝驰
作者单位:沈阳航空航天大学 航空航天工程学部(院 )辽宁省航空推进系统先进测试技术重点实验室, 沈阳 110136
基金项目:中航产学研创新基金(cxy2013SH17)
摘    要:为实现对该类复合材料部件结构完整性的设计分析,以连续纤维增强复合材料轴结构为研究对象,对比分析4种细观力学模型计算连续纤维增强金属基复合材料的力学性能参数;在此基础上,采用RVE(代表体积元)有限元模型计算的复合材料力学性能参数作为输入,建立连续纤维增强金属基复合材料轴结构力学分析模型.计算与对比分析不同材料方案下纤维增强金属基复合材料轴结构在扭转载荷作用下的变形量及承扭能力,当纤维体积分数一定时,方案4的变形量最小,方案2的临界屈曲转矩最大. 

关 键 词:连续纤维增强复合材料    低压涡轮轴    细观力学方法    变形量    屈曲转矩
收稿时间:9/4/2014 12:00:00 AM

Analysis on torsional feature of continuous fiber reinforced metal matrix composite turbine shaft
SHA Yun-dong,JIA Que-yue,LUO Li,ZHAO Feng-tong and LUAN Xiao-chi.Analysis on torsional feature of continuous fiber reinforced metal matrix composite turbine shaft[J].Journal of Aerospace Power,2016,31(6):1377-1384.
Authors:SHA Yun-dong  JIA Que-yue  LUO Li  ZHAO Feng-tong and LUAN Xiao-chi
Institution:Liaoning Key Laboratory of Advanced Measurement and Test Technology for Aviation Propulsion System, Faculty of Aerospace Engineering, Shenyang Aerospace University, Shenyang 110136, China
Abstract:To realized design and analysis of composite parts structural integrity, the low pressure turbine shaft was taken as the object of research. Firstly, four kinds of micromechanical methods were utilized to calculate the mechanical parameter of continuous filament reinforced metal matrix composite. Secondly,the calculated parameters of RVE (representative volume element) finite element model were taken as input and the mechanics analysis model of fiber reinforced metal matrix composite shaft was built. The optimal solution could be got by calculating the deformation and bearing capacity of continuous filament reinforced metal matrix composite shaft with torsion load and by comparing with the deformation and bearing capacity of shaft with different laminate schemes; in case of certain fiber volume fraction, the deformation of scheme 4 is the smallest, and the critical buckling torque of scheme 2 is the greatest.
Keywords:continuous filament reinforced composite materials  low pressure turbine shaft  micromechanical method  deformation  bucking torque
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