Study on Hydrogen Combustors with Two-Staged Combustion Method for Micro Gas Turbines (Combustion Characteristics of Coaxial Type Injectors)-Reference-Cited by-同舟云学术

Study on Hydrogen Combustors with Two-Staged Combustion Method for Micro Gas Turbines (Combustion Characteristics of Coaxial Type Injectors)

Published:2007 Issue:3 Volume:2 Page:590-600
ISSN:1880-988X
Container-title:Journal of Environment and Engineering
language:en
Short-container-title:JEE

Author:

MINAKAWA Katsuhiro¹,YUASA Saburo¹

Affiliation:

1. Tokyo Metropolitan Institute of Technology

Publisher

Japan Society of Mechanical Engineers

Subject

General Medicine

Link

http://www.jstage.jst.go.jp/article/jee/2/3/2_3_590/_pdf

Reference13 articles.

1. Combustion Performance of a Hydrogen-fueled Small Combustor for a Micro Gas Turbine.

2. (2) Yuasa, S., Nishida, K., Shigeta, M. and Minakawa, K., Combustion Characteristics of a Premixed Test Combustor for a Hydrogen-Fueled Micro Gas Turbine, Transactions of the Japan Society of Mechanical Engineers, Series B, Vol. 61, No. 558 (1995), pp. 3075-3081.

3. (3) Minakawa, K., Akizuki, W., Goto, N. and Yuasa, S., Development of a Lean Premixed-Type Combustor with a Divergent Flameholder for a Hydrogen-Fueled Micro Gas Turbine, Proceedings of the 14th International Symposium on Air Breathing Engines, (1999-9), ISABE 99-7010.

4. (4) Kobayashi, K., Waku, Y., Nakagawa, N. and Yokoi, S., Technology Research on High Efficiency Gas Turbine Utilizing Melt-Growth Composite Ceramics, Proceedings of the Yokohama International Gas Turbine Congress, (2003-11), TS-125.

5. (5) Enzaki, Y. and Kuyama, T., Trend of Dry Low NOx Combustor Development -Aircrafts-, Journal of the Gas Turbine Society of Japan, Vol. 23, No. 89 (1995), pp. 31-38.

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