1) radial turbines
径向透平
2) variable geometry radial inflow turbine
变几何径向透平
1.
Loss models and loss analysis of variable geometry radial inflow turbine;
变几何径向透平损失模型及其分析
3) centrifugal turbocompressor
径向透平压缩机(radial turbo-compressor)
4) Inflow Turbine
径流透平
5) radial inflow turbine
向心透平
1.
The mathematical model of design and calculation for radial inflow turbine was established on the basis of studying structure features and working principle of radial inflow turbine for micro gas turbine generator.
在研究微型燃气轮机向心透平结构特点和工作原理的基础上,建立了向心透平设计计算的数学模型。
2.
Tip clearance flow in a radial inflow turbine rotor blade under stage environment was investigated by 3-dimensional viscous flow simulation.
对微型燃机向心透平叶轮顶部间隙流动在级环境下进行了全三维粘性数值模拟。
3.
The general design principles on shape-design of radial inflow turbine guide vanes were discussed.
对微型燃气轮机向心透平导向器叶片型线的设计原则进行了探讨,设计出了5种尾缘厚度的导向器叶片,并分别对其通道流场进行了全三维黏性数值模拟。
6) centripetal turbine
向心透平
1.
For the purpose of developing micro-gas-turbines of 100 kW capacity,a high speed precision performance test rig for centripetal turbines has been designed and built.
为开发100 kW微型燃气轮机,自主设计建造了高速高精度向心透平性能试验装置。
2.
The blade design of centripetal turbine is introduced in this paper,and some design skills are also discussed.
介绍向心透平叶片的造型设计及探讨一些设计技
补充资料：径向透平压缩机(radial turbo-compressor)
分子式：
CAS号：
性质：又称径向透平压缩机(radial turbo-compressor)。利用离心力为推动力的一类透平压缩机。气体沿径向流动。排气压力可达到34.3MPa(350kgf/cm2)以上。见透平压缩机。
CAS号：
性质：又称径向透平压缩机(radial turbo-compressor)。利用离心力为推动力的一类透平压缩机。气体沿径向流动。排气压力可达到34.3MPa(350kgf/cm2)以上。见透平压缩机。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条