中文摘要：

An increase of the cooling capacities in the liquid helium temperature area is required by Experimental Advanced Superconducting Tokamak(EAST) due to the extension of its subsystems in the near future.Limited by the heat exchangers,cryogenic pipes,and cryogenic valves,it is difficult to enlarge the present EAST helium system.10~2 W@4.5 K level helium cryogenic systems are needed in view of feasibility and economy.A turboexpander is the key component of a helium cryogenic system.In this article,a hydrostatic gas lubricated cryogenic helium turboexpander for a 900 W@4.5 K cryogenic helium system was developed for the EAST updated subsystem by the Institute of Plasma Physics,Chinese Academy of Sciences and the Institute of Cryogenic and Refrigeration of Xi’an Jiaotong University.The main components,such as gas bearings,expansion wheel,shaft,and brake wheel,were briefly presented.The dynamic performance of the journal and thrust gas bearings was investigated numerically.The rotordynamic performance of the developed turboexpander was studied experimentally.The results show that the axial and radial load capacities supplied by the journal gas bearing and thrust gas bearing are enough to balance the axial force and radial force of the rotor.A 43%overspeed operation was achieved,which validated the reasonable design of the turboexpander.

英文摘要：

An increase of the cooling capacities in the liquid helium temperature area is re- quired by Experimental Advanced Superconducting Tokamak （EAST） due to the extension of its subsystems in the near future. Limited by the heat exchangers, cryogenic pipes, and cryogenic valves, it is difficult to enlarge the present EAST helium system. 102 W@4.5 K level helium cryogenic systems are needed in view of feasibility and economy. A turboexpander is the key com- ponent of a helium cryogenic system. In this article, a hydrostatic gas lubricated cryogenic helium turboexpander for a 900 W@4.5 K cryogenic helium system was developed for the EAST updated subsystem by the Institute of Plasma Physics, Chinese Academy of Sciences and the Institute of Cryogenic and Refrigeration of Xi＇an Jiaotong University. The main components, such as gas bearings, expansion wheel, shaft, and brake wheel, were briefly presented. The dynamic perfor- mance of the journal and thrust gas bearings was investigated numerically. The rotordynamic performance of the developed turboexpander was studied experimentally. The results show that the axial and radial load capacities supplied by the journal gas bearing and thrust gas bearing are enough to balance the axial force and radial force of the rotor. A 43% overspeed operation was achieved, which validated the reasonable design of the turboexpander.