Abstract
For the contribution to the development of FJR710, high by-pass ratio turbofan engine, with the study for many years of the development of high efficiency turbine for the jet engine, the first technical prize from the Energy Resource Research Committee was awarded in April, 1988. This report introduced its technical contents. In order to improve the thermal efficiency and enlarge the output, it is very effective to raise the gas temperature at the inlet of gas turbine. For its purpose, by cooling the nozzle and moving blades and having those blades operate at lower temperature than that of the working limitation, they realized, for the first time in Japan, the technique of cooling turbine to heighten the operational gas temperature. By that technique, it was enabled to raise the gas temperature at the inlet of turbine, to 1,350/sup 0/C from 850/sup 0/C. This report explain many important points of study covering the basic test, visualizing flow experiment, material discussion and structural design in the process of development. (9 figs)
Citation Formats
Takahara, Kitao, Nouse, Hiroyuki, Yoshida, Toyoaki, Minoda, Mitsuhiro, Matsusue, Katsutoshi, and Yanagi, Ryoji.
Development of high temperature turbine.
Japan: N. p.,
1988.
Web.
Takahara, Kitao, Nouse, Hiroyuki, Yoshida, Toyoaki, Minoda, Mitsuhiro, Matsusue, Katsutoshi, & Yanagi, Ryoji.
Development of high temperature turbine.
Japan.
Takahara, Kitao, Nouse, Hiroyuki, Yoshida, Toyoaki, Minoda, Mitsuhiro, Matsusue, Katsutoshi, and Yanagi, Ryoji.
1988.
"Development of high temperature turbine."
Japan.
@misc{etde_6665414,
title = {Development of high temperature turbine}
author = {Takahara, Kitao, Nouse, Hiroyuki, Yoshida, Toyoaki, Minoda, Mitsuhiro, Matsusue, Katsutoshi, and Yanagi, Ryoji}
abstractNote = {For the contribution to the development of FJR710, high by-pass ratio turbofan engine, with the study for many years of the development of high efficiency turbine for the jet engine, the first technical prize from the Energy Resource Research Committee was awarded in April, 1988. This report introduced its technical contents. In order to improve the thermal efficiency and enlarge the output, it is very effective to raise the gas temperature at the inlet of gas turbine. For its purpose, by cooling the nozzle and moving blades and having those blades operate at lower temperature than that of the working limitation, they realized, for the first time in Japan, the technique of cooling turbine to heighten the operational gas temperature. By that technique, it was enabled to raise the gas temperature at the inlet of turbine, to 1,350/sup 0/C from 850/sup 0/C. This report explain many important points of study covering the basic test, visualizing flow experiment, material discussion and structural design in the process of development. (9 figs)}
journal = []
volume = {9:4}
journal type = {AC}
place = {Japan}
year = {1988}
month = {Jul}
}
title = {Development of high temperature turbine}
author = {Takahara, Kitao, Nouse, Hiroyuki, Yoshida, Toyoaki, Minoda, Mitsuhiro, Matsusue, Katsutoshi, and Yanagi, Ryoji}
abstractNote = {For the contribution to the development of FJR710, high by-pass ratio turbofan engine, with the study for many years of the development of high efficiency turbine for the jet engine, the first technical prize from the Energy Resource Research Committee was awarded in April, 1988. This report introduced its technical contents. In order to improve the thermal efficiency and enlarge the output, it is very effective to raise the gas temperature at the inlet of gas turbine. For its purpose, by cooling the nozzle and moving blades and having those blades operate at lower temperature than that of the working limitation, they realized, for the first time in Japan, the technique of cooling turbine to heighten the operational gas temperature. By that technique, it was enabled to raise the gas temperature at the inlet of turbine, to 1,350/sup 0/C from 850/sup 0/C. This report explain many important points of study covering the basic test, visualizing flow experiment, material discussion and structural design in the process of development. (9 figs)}
journal = []
volume = {9:4}
journal type = {AC}
place = {Japan}
year = {1988}
month = {Jul}
}