Z
Zhu Yangli
Researcher at Chinese Academy of Sciences
Publications - 44
Citations - 157
Zhu Yangli is an academic researcher from Chinese Academy of Sciences. The author has contributed to research in topics: Turbine & Compressed air energy storage. The author has an hindex of 4, co-authored 44 publications receiving 110 citations.
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Compressed air electric power energy storage system
TL;DR: In this paper, the authors proposed a compressed air electric power energy storage system achieving hydraulic and pneumatic coupling, where a compressor unit compresses air into a constant-pressure air storage device, liquid in the constant voltage air storage devices is compressed into a variable-pressure storage device through a liquid pump, and accordingly electric energy is converted to air and liquid internal energy for storage.
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Experimental and Numerical investigation of closed Radial-Inflow Turbine with Labyrinth Seals
TL;DR: In this article, an experimental and computational investigation of shroud clearance flow in a radial inflow turbine with labyrinth seals is presented, showing that the labyrinth seal flow has no effect on the main flow passage and mainly causes different leakage mass flow.
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Effect of blade tip leakage flow on erosion of a radial inflow turbine for compressed air energy storage system
TL;DR: In this paper, the effects of tip leakage flow on erosion of a CAES radial inflow turbine are investigated at different tip clearances and total pressure ratios, showing that the region with higher erosion rate on the shroud of rotor gradually extends to downstream.
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Flow characteristic of a multistage radial turbine for supercritical compressed air energy storage system
TL;DR: In this paper, a supercritical compressed air energy storage system expand from supercritical to atmospheric conditions at lower inlet temperature (<500 k) to generate MW-scale power, and the system is used to store the compressed air.
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Flow analysis and performance improvement of a radial inflow turbine with back cavity under variable operation condition of compressed air energy storage
TL;DR: In this paper, the effect of back cavity in a radial inflow turbine is investigated numerically, and the size effect of labyrinth seal clearance is revealed, and performances of radial turbine with back cavity at different total expansion ratio are also investigated.