국내 최대 기계 및 로봇 연구정보

기술보고서

기술보고서 게시판 내용
타이틀	Research and Development of Combustors for Gas Turbine and Jet Engines in the National Aerospace Laboratory
저자	Takashi TAMARU
Keyword	gas turbine; jet engine; combustor; combustion chambar; FJR710
URL	http://send.nal.go.jp/send/jpn/dlfile.php3/naltm00676?doctype=6&filetype=20&path0=naltm00676&path1=pdf&path2=naltm00676.pdf
보고서번호	NAL TM-676
발행년도	1995.1
출처	NAL (National Aerospace Laboratory of Japan)
ABSTRACT	The basic technology and experiences in the National Aerospace Laboratory for the development of gas turbine combustors are described.Particular emphasis is placed on the combustor development for the turbofan engine FJR710 for a short take-off and landing plane and on the high efficiency gas turbine,AGTJ-100A,for use as a power plant.Basic experimental techniques and knowledge for research and development of the gas turbine combustors are also described