Characterization of Combustion Processes of Fuel Sprays Injected into High-Temperature and High-Speed Airstream
Characterization of Combustion Processes of Fuel Sprays Injected into High-Temperature and High-Speed Airstream
批准号:
04452149
负责人:
HIROYASU Hiroyuki
金额:
$0.38万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for General Scientific Research (B)
财政年份:
1992
资助国家:
日本
项目状态:
已结题
起止时间:
1992 至 1993
中文摘要
对高温高速气流中煤油喷雾的特性过程进行了实验研究。燃烧室的内部具有70mm x 70mm的矩形横截面。在燃烧室横截面的中心处,从喷嘴向下一定距离(混合距离)处,设置了一个矩形钝体。今年的试验是由燃烧室两侧各喷入四股喷雾进行的。喷嘴在燃烧室两侧的位置改变了喷雾在气流中的分布。主要结果如下。(1)A火焰熄灭的临界煤油流量随气流温度先减小后增大,但变化不大。(2)当气流温度和煤油流量较高时,在混合距离(旋流喷嘴与海崖体之间)处发现喷雾自燃。随着气流温度的升高,自燃临界煤油流量减小,稳定燃烧范围变窄。(3)燃烧室中相对均匀的喷雾分布使火焰熄灭和自燃的临界煤油流量增大。由于自燃临界煤油流量随气流温度的增加大于火焰熄灭临界煤油流量随气流温度的增加,使得稳定燃烧范围变宽。(4)混合长度对火焰熄灭的临界煤油流量影响不大。混合长度的增加降低了自燃的临界煤油流量。
英文摘要
An experimental study was conducted on the characterization processes of kerosene sprays injected into a high-temperature and high-speed airstream. The interior of the combustor has a rectangular cross-section of 70mm x 70mm. A bluffbody with a rectangular shape was settled at the center of the cross section of the combustor which was a certain distance(mixing distance)down the airstream from the nozzle. The experiment in this year was made of the combustion of four sprays injected from each side of the combustor. A distribution of the sprays in the airstream was changed by the location of the nozzle on each side of the combustor. Main results obtained are as follows.(1)A critical kerosene flow rate for flame blow off was decreased and then increased with the airstream temperature, but the variation was small.(2)Spontaneous ignition of the sprays at the mixing distance(between the swirl nozzles and the bluff body)was found when both the airstream temperature and the kerosene flow rate were high. A decrease in a critical kerosene flow rate for the spontaneous ignition with an increase in the airstream temperature made stable combustion range narrow.(3)Relatively homogenizing a distribution of the sprays in the combustor increased the critical kerosene flow rates for both the flame blow off and the spontaneous ignition. A stable combusion range was made wide since the increase with the airstream temperature in the critical kerosene flow rate for the spontaneous ignition was larger than that for the flame blow off.(4)The mixing length did not have a large effect on the critical kerosene flow rate for the flame blow off. An increase in the mixing length reduced the critical kerosene flow rate for the spontaneous ignition.
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小田 哲也: "レーザーライトシートによる燃料噴霧の断面写真撮影法" 日本航空宇宙学会西部支部講演会(1992)講演集. 141-144 (1992)
Tetsuya Oda:“使用激光光片的燃料喷射的横截面拍摄方法”日本航空学会西部分会论文集(1992)141-144(1992)。
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小田哲也: "高速気流中における液体噴流の微粒化特性(液滴の直径,速度と液体噴流の分裂挙動の関係)" 日本機械学会第71期全国大会講演論文集. D. 168-170 (1993)
Tetsuya Oda:“高速气流中液体射流的雾化特性(液滴直径、速度和液体射流破碎行为之间的关系)”第 71 届日本机械工程师学会全国会议论文集 D. 168-170(1993 年)。 ) )
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ODA,Tetsuya: "Characteristics of Liquid Jet Atomization across a High-Speed Airstream(Relation between Drop Diameter and Velocity with Breakup Behavior of Liquied Jet)(in Japanese)" Proceedings of the 71st JSME Fall Annual Meeting. Vol.D. 168-170
ODA、Tetsuya:“高速气流中液体射流雾化的特性(液滴直径和速度与液体射流破碎行为的关系)(日语)”第 71 届 JSME 秋季年会论文集。
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ODA,Tetsuya: "Characteristics of Liquid Jet Atomization Across a High-Speed Airstream(to be presented)" Proceedings of Sixth International Conference on Liquid Atomization and Spray Systems(ICLASS-94). (1994)
ODA,Tetsuya:“高速气流中液体射流雾化的特征(待提交)”第六届国际液体雾化和喷雾系统会议(ICLASS-94)会议记录。
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小田哲也: "気泡混入による高速気流中の噴霧の分散特性の制御" 日本航空宇宙学会西部支部講演会(1993)講演集. 120-123 (1993)
Tetsuya Oda:“通过混合气泡控制高速气流中喷雾的分散特性”日本航空学会西部分会会议记录(1993)120-123(1993)。
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共 17 条
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Combustion of Fuel Spray Injected into High Speed Airstream
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