首页> 外文期刊>Russian Aeronautics >Development of Methods for Designing Turbines and Compressors as a Part of Gas Turbine Engines
【24h】

Development of Methods for Designing Turbines and Compressors as a Part of Gas Turbine Engines

机译:开发涡轮机和压缩机作为燃气涡轮发动机一部分的设计方法

获取原文
获取原文并翻译 | 示例
           

摘要

The results of refining the known methods and developing new ones are presented for selecting and optimizing the main parameters of turbochargers in the design of gas turbine engines. Methods have been developed for determining the optimal number of stages, placing points for stages on the Smith charts, changing the work along the height of the flow path and the geometry of turbine and compressor elements.
机译:提出了改进已知方法和开发新方法的结果,以用于选择和优化燃气涡轮发动机设计中涡轮增压器的主要参数。已经开发了用于确定最佳级数的方法,在史密斯圆图上放置级点,沿流路高度改变功以及涡轮机和压缩机元件的几何形状。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号