Volume 31 Issue 6
Jun.  2016
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SHA Yun-dong, JIA Que-yue, LUO Li, ZHAO Feng-tong, 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. doi: 10.13224/j.cnki.jasp.2016.06.013
Citation: SHA Yun-dong, JIA Que-yue, LUO Li, ZHAO Feng-tong, 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. doi: 10.13224/j.cnki.jasp.2016.06.013

Analysis on torsional feature of continuous fiber reinforced metal matrix composite turbine shaft

doi: 10.13224/j.cnki.jasp.2016.06.013
  • Received Date: 2014-09-04
  • Publish Date: 2016-06-28
  • 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.

     

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