7 Papers
14 Citations
Dan Luo is an academic researcher from University of Shanghai for Science and Technology. The author has contributed to research in topics: Turbine & Overall pressure ratio. The author has an hindex of 2, co-authored 4 publications.
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Papers
The design and analysis of supercritical carbon dioxide centrifugal turbine
TL;DR: In this article, a 10MW single-stage SCO 2 working fluid was designed and the unsteady three-dimensional flow field inside the blade passages was assessed by software CFX to obtain the desired parameters of the turbine with maximum total static efficiency.
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Energy performance of a rural residential building with PCM-silica aerogel sunspace in severe cold regions
TL;DR: In this article , a sunspace for rural residential buildings using PCM walls and silica aerogel glass (PCMS-silica) to reduce indoor temperature fluctuations in cold regions was proposed.
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Design and performance analysis of three stage centrifugal turbine
Dan Luo,Xin Tan,Diangui Huang +2 more
TL;DR: In this article, a three-stage centrifugal turbine was designed based on the thermodynamic parameters of a four-stage test axial turbine, and the results showed that the key simulation parameters including total-static efficiency, shaft power, reaction degree, velocity ratio and pressure ratio of turbine stages are close to the 1D calculation values; at the design condition, streamline is smooth in the passage of turbine cascades.
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Design of 1 + 1 / 2 counter rotating centrifugal turbine and performance comparison with two-stage centrifugal turbine
TL;DR: In this article, the authors applied the counter-rotating turbine technology to the centrifugal turbine and carried out the aerodynamic design of the 1 + 1/2 counterrotating cyclic turbine stage using the air ideal gas as the working fluid.
6
Patent
Combustion gas turbine
Huang Diangui,Tan Xin,Li Yin Ge,Chen Cheng,Wang Zhu,Wang Nai'an,Lin Xianqiao,Zhu Wendu,Pang Yumeng,Dan Luo,Chen Xiaogang,Shao Shengbo,Yu Yifan,Liu Lanyi +13 more
- 30 Sep 2015
TL;DR: In this article, a combustion gas turbine is characterized by comprising a spindle, radial inflow compressors, combustion chambers, an outward flow turbine and a shell, and the shell comprises compressor shell bodies, combustion chamber shell bodies and a turbine shell.
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