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首页|期刊导航|热科学学报(英文版)|Influence Factors for Impact Actions and Transient Trajectories of Fan Blades after Fan Blade Out in Typical 2-Shaft High Bypass Ratio Turbofan Engine

Influence Factors for Impact Actions and Transient Trajectories of Fan Blades after Fan Blade Out in Typical 2-Shaft High Bypass Ratio Turbofan Engine

XU Xue LI Hongxin FENG Guoquan

热科学学报(英文版)2022,Vol.31Issue(1):96-110,15.
热科学学报(英文版)2022,Vol.31Issue(1):96-110,15.

Influence Factors for Impact Actions and Transient Trajectories of Fan Blades after Fan Blade Out in Typical 2-Shaft High Bypass Ratio Turbofan Engine

Influence Factors for Impact Actions and Transient Trajectories of Fan Blades after Fan Blade Out in Typical 2-Shaft High Bypass Ratio Turbofan Engine

XU Xue 1LI Hongxin 2FENG Guoquan1

作者信息

  • 1. Shenyang Engine Research Institute,Aero Engine Corporation of China,Shenyang 110015,China
  • 2. Corporation Headquarter,Aero Engine Corporation of China,Beijing 100097,China
  • 折叠

摘要

关键词

fan blade out/transient trajectory/design character/structural fuse/high bypass ratio/turbofan

Key words

fan blade out/transient trajectory/design character/structural fuse/high bypass ratio/turbofan

引用本文复制引用

XU Xue,LI Hongxin,FENG Guoquan..Influence Factors for Impact Actions and Transient Trajectories of Fan Blades after Fan Blade Out in Typical 2-Shaft High Bypass Ratio Turbofan Engine[J].热科学学报(英文版),2022,31(1):96-110,15.

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