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CEC-ICMC 2015 - Timetable, Abstracts and Presentations Contribution ID : 119 Type : Poster Presentation The Study of Flow Performance inside a High-speed Radial-axial Flow Cryogenic Turbo-expander impeller Abstract content In this paper, an optimization design for whole performance of a high-speed radial-axial flow cryogenic turbo-expander is discussed. The main structural parameters of the expander blade are obtained through a design method based on one-dimension steady flow. The non –developable ruled parabolic shaping method is used to design the leaf type. Then numerical simulation and detailed analysis are carried out based on the designed turbine with its given working condition using CFD software. At last the temperature field, pressure field, streamlines and isentropic efficiency are obtained, and the optimization design including the geometry of impellers and boundary conditions for an efficient turbo-expander is achieved. Primary author(s) : MENG, Yanrong (The Technical Institute of Physics and Chemistry,CAS) Co-author(s) : Dr. XIONG, Lianyou (TIPC); LIU, Liqiang (Technical Institute of Physics and Chemistry of CAS-Academia Si); PENG, Nan; LI, Kongrong (Technical Institute of Physics and Chemistry,CAS) Presenter(s) : Dr. XIONG, Lianyou (TIPC) Session Classification : C3PoE - Turbomachines and Helium Components Track Classification : CEC-05 - Expanders, Pumps, Compressors, and Regenerators

The Study of Flow Performance Inside a High-speed Radial-Axial Flow Cryogenic Turbo-expander Impeller - Contribution

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Page 1: The Study of Flow Performance Inside a High-speed Radial-Axial Flow Cryogenic Turbo-expander Impeller - Contribution

CEC-ICMC 2015 - Timetable, Abstracts and Presentations

Contribution ID : 119 Type : Poster Presentation

The Study of Flow Performance inside a High-speedRadial-axial Flow Cryogenic Turbo-expander impeller

Abstract contentIn this paper, an optimization design for whole performance of a high-speed radial-axial flow cryogenicturbo-expander is discussed. The main structural parameters of the expander blade are obtainedthrough a design method based on one-dimension steady flow. The non –developable ruled parabolicshaping method is used to design the leaf type. Then numerical simulation and detailed analysis arecarried out based on the designed turbine with its given working condition using CFD software. Atlast the temperature field, pressure field, streamlines and isentropic efficiency are obtained, and theoptimization design including the geometry of impellers and boundary conditions for an efficientturbo-expander is achieved.

Primary author(s) : MENG, Yanrong (The Technical Institute of Physics and Chemistry,CAS)

Co-author(s) : Dr. XIONG, Lianyou (TIPC); LIU, Liqiang (Technical Institute of Physics andChemistry of CAS-Academia Si); PENG, Nan; LI, Kongrong (Technical Institute of Physics andChemistry,CAS)

Presenter(s) : Dr. XIONG, Lianyou (TIPC)

Session Classification : C3PoE - Turbomachines and Helium Components

Track Classification : CEC-05 - Expanders, Pumps, Compressors, and Regenerators