Development of compressor for ultra micro gas turbine

被引:4
作者
Mizuki, Shimpei [1 ]
机构
[1] Hosei Univ, Fac Engn, Dept Mech Engn, Tokyo 1848584, Japan
关键词
ultra micro gas turbine; ultra micro centrifugal compressor;
D O I
10.1007/s11630-007-0019-2
中图分类号
O414.1 [热力学];
学科分类号
摘要
The major problems for the development of an ultra micro gas turbine system were discussed briefly from the stand point of the internal flow and the performance characteristics. Following to these, the development of ultra micro centrifugal compression systems for the ultra micro gas turbine is explained with the design and the manufacturing processes. The measured results of ultra micro centrifugal compressors are shown.
引用
收藏
页码:19 / 27
页数:9
相关论文
共 12 条
[1]  
AKIYAMA T, 2006, THESIS HOSEI U
[2]   Microengineering - Macro power from micro machinery [J].
Epstein, AH ;
Senturia, SD .
SCIENCE, 1997, 276 (5316) :1211-1211
[3]  
HIRANO T, 2006, ISROMAC112006135
[4]  
HIRANO T, 2005, ACGT2005062
[5]  
HIRANO T, 2005, P 7 ISAIF TOK, V1, P71
[6]  
ISOMURA K, 2002, 8 POW EN TECHN S JSM
[7]  
NAGASAKI T, 2005, J JAPAN I ENERGY, V84, P221
[8]  
*NEDO INT COLL, 2001, 51101591 NEDO INT CO
[9]  
Nowak R. J., 2000, DARPAS ADV ENERGY TE
[10]  
SINGER R, 1998, MEMS SOLDIER SYSTEMS