热科学学报（英文版）2008，Vol.17Issue(1)：28-34,7.
Turbo-pump with Isolated Two Stage Impellers for Future Rocket Engine (Trial to Drive Impellers Independently)
Turbo-pump with Isolated Two Stage Impellers for Future Rocket Engine (Trial to Drive Impellers Independently)
Toshiaki Kanemoto 1Makoto Shimojyo 1Ryunosuke Kawashima 1Daisuke Tanaka 2Akira Inagaki 2Shin Oba2
作者信息
- 1. Kyushu Institute of Technology: Sensui 1-1, Tobata, Kitakyushu 804-8550, Japan
- 2. DMW Corporation: Miyoshi 3-27, Mishima 411-8560, Japan
- 折叠
摘要
Abstract
To suppress the cavitation in the impellers and to make the turbo-pump lives longer, the inducer was separated from the main impeller and both impellers were driven independently. The performance of the pump and the flow conditions around the impellers were investigated experimentally and the following results were obtained.(1)The main impeller contributes to the flow interaction between the inducer and the main impeller. (2)The rotational speeds of both impellers can be controlled independently in order to suppress simultaneously the cavitation not only in the main impeller, but also in the inducer.关键词
Turbo-pump, Inducer, Impeller, Rocket Engine, Cavitation, NPSHKey words
Turbo-pump, Inducer, Impeller, Rocket Engine, Cavitation, NPSH分类
数理科学引用本文复制引用
Toshiaki Kanemoto,Makoto Shimojyo,Ryunosuke Kawashima,Daisuke Tanaka,Akira Inagaki,Shin Oba..Turbo-pump with Isolated Two Stage Impellers for Future Rocket Engine (Trial to Drive Impellers Independently)[J].热科学学报（英文版）,2008,17(1):28-34,7.
