杨帆1,张大海2,范顺昌3.骨架式压气机机匣仿真计算分析[J].航空发动机,2017,43(4):30-34
骨架式压气机机匣仿真计算分析
Simulation Analysis of a Compressor Casing of Skeletal Supporting Frame Structure
  
DOI:
中文关键词:  推重比  骨架式结构  压气机机匣  仿真  航空发动机
英文关键词:thrust-weight ratio  skeletal supporting frame structure  compressor casing  simulation aeroengine
基金项目:航空动力基础研究项目资助
作者单位E-mail
杨帆1,张大海2,范顺昌3 1. 中国航发沈阳发动机研究所沈阳1100152. 解放军93115 部队沈阳110031 3. 空军驻沈阳黎明航空发动机(集团)有限责任公司军事代表室沈阳110015 yangfan01234@163.com 
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中文摘要:
      为了实现通过改变压气机机匣材料、结构形式和加工手段,达到减轻压气机机匣质量的目标,依照骨架式结构设计思 想,对某型压气机的机匣进行了骨架式结构的改进设计,即“桁架”式结构机匣,并针对这3 种典型的结构机匣分别从静强度、模态 和包容特性等角度进行了仿真计算和对比分析,得到了现阶段最优方案为圆形开孔机匣。结果表明:该类骨架结构可以实现在不影 响机匣使用要求的前提下,将压气机机匣质量减轻10%~20%,有效提高发动机推重比。
英文摘要:
      In order to reduce the compressor casing weight by changing the casing material, structure form and manufacturing method, according to the principle of the skeletal supporting frame structure, the improved design of skeletal supporting frame structure for a compressor casing was conducted, which was truss structure. The simulation and comparative analysis of three kinds of typical structure casing were performed respectively from the static stress, mode and containment capability, and the best scheme was obtained at present that was circular opening casing. The result shows that the skeletal supporting frame should reduce the compressor weight as 10%~20% to improve the engine thrust-weight ratio, which has no influence on casing application requirement.
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