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Fiscal 1998 research report. R and D on advanced combustion technology under microgravity environment; 1998 nendo seika hokokusho. Bisho juryoku kankyo wo riyoshita kodo nensho gijutsu soshutsu ni kansuru kenkyu kaihatsu

Abstract

Research was made on explication of a combustion phenomenon by using a microgravity facility, and a combustor possible to realize advanced combustion technology. In the basic research composed of 5 themes by the international joint research with NASA, 52 drop experiments using JAMIC's facility and 100 drop experiments using NASA's 2.2s drop tower were carried out. The themes are composed of an interaction in droplet arrays combustion, combustion of binary fuel sprays, combustion characteristics of solid fuel, flame dynamics around a lean flammability limit, and mass transfer around a combustion field. In the experiment using the microgravity experiment facility and analysis evaluation of the experimental data, studies were made on combustion and evaporation of fuel droplets, combustion characteristics of dense fuel, flammability limit, formation mechanism of NO{sub x} and an advanced combustor. For applying a pre-evaporating/pre- mixing combustion system to a combustor for aircraft engines, studies were made on some issues such as improvement of a combustion stability, NO{sub x} discharge characteristics, and optimum fuel atomizing. (NEDO)
Authors:
"NONE"
Publication Date:
Mar 01, 1999
Product Type:
Technical Report
Report Number:
JP-NEDO-010013645
Resource Relation:
Other Information: PBD: Mar 1999
Subject:
42 ENGINEERING; WEIGHTLESSNESS; COMBUSTION; COMBUSTORS; NASA; FUELS; DROPLETS; SOLID FUELS; NITROGEN OXIDES; AIRCRAFT; ENGINES
OSTI ID:
20029231
Research Organizations:
New Energy and Industrial Technology Development Organization, Tokyo (Japan)
Country of Origin:
Japan
Language:
Japanese
Other Identifying Numbers:
TRN: JN9940236
Availability:
Available to ETDE participating countries only(see www.etde.org); commercial reproduction prohibited; OSTI as DE20029231
Submitting Site:
NEDO
Size:
378 pages
Announcement Date:

Citation Formats

Fiscal 1998 research report. R and D on advanced combustion technology under microgravity environment; 1998 nendo seika hokokusho. Bisho juryoku kankyo wo riyoshita kodo nensho gijutsu soshutsu ni kansuru kenkyu kaihatsu. Japan: N. p., 1999. Web.
Fiscal 1998 research report. R and D on advanced combustion technology under microgravity environment; 1998 nendo seika hokokusho. Bisho juryoku kankyo wo riyoshita kodo nensho gijutsu soshutsu ni kansuru kenkyu kaihatsu. Japan.
1999. "Fiscal 1998 research report. R and D on advanced combustion technology under microgravity environment; 1998 nendo seika hokokusho. Bisho juryoku kankyo wo riyoshita kodo nensho gijutsu soshutsu ni kansuru kenkyu kaihatsu." Japan.
@misc{etde_20029231,
title = {Fiscal 1998 research report. R and D on advanced combustion technology under microgravity environment; 1998 nendo seika hokokusho. Bisho juryoku kankyo wo riyoshita kodo nensho gijutsu soshutsu ni kansuru kenkyu kaihatsu}
abstractNote = {Research was made on explication of a combustion phenomenon by using a microgravity facility, and a combustor possible to realize advanced combustion technology. In the basic research composed of 5 themes by the international joint research with NASA, 52 drop experiments using JAMIC's facility and 100 drop experiments using NASA's 2.2s drop tower were carried out. The themes are composed of an interaction in droplet arrays combustion, combustion of binary fuel sprays, combustion characteristics of solid fuel, flame dynamics around a lean flammability limit, and mass transfer around a combustion field. In the experiment using the microgravity experiment facility and analysis evaluation of the experimental data, studies were made on combustion and evaporation of fuel droplets, combustion characteristics of dense fuel, flammability limit, formation mechanism of NO{sub x} and an advanced combustor. For applying a pre-evaporating/pre- mixing combustion system to a combustor for aircraft engines, studies were made on some issues such as improvement of a combustion stability, NO{sub x} discharge characteristics, and optimum fuel atomizing. (NEDO)}
place = {Japan}
year = {1999}
month = {Mar}
}