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Effect of Fuel Injector Type on Performance and Emissions of Reverse-Flow Combustor

机译：燃油喷射器类型对逆流燃烧器性能和排放的影响

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摘要

The combustion process in a reverse-flow combustor suitable for a small gas turbine engine was investigated to evaluate the effect of fuel injector type on performance and emissions. Fuel injector configurations using pressure-atomizing, spill-flow, air blast, and air-assist techniques were compared and evaluated on the basis of performance obtained in a full-scale experimental combustor operated at inlet conditions corresponding to takeoff, cruise, low power, and idle and typical of a 16:1-pressure-ratio turbine engine. Major differences in combustor performance and emissions characteristics were experienced with each injector type even though the aerodynamic configuration was common to most combustor models. Performance characteristics obtained with the various fuel injector types could not have been predicted from bench-test injector spray characteristics. The effect of the number of operating fuel injectors on performance and emissions is also presented.

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作者
Norgren, C. T.; Riddlebaugh, S. M.;
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年度 1981
页码 p.1-40
总页数 40
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Combustion chambers; Fuel injection; Gas turbine engines; Performance tests; Engine tests; Helicopters; Injectors; Jet engines;

机译：燃烧室;燃油喷射;燃气涡轮发动机;性能试验;发动机试验;直升机;喷油器;喷气发动机;

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专利

1. Influence of combustor inlet conditions on combustor exit gas peak temperature factor (experiment by using the combustor with pressure atomizing fuel nozzles and the combustor with airblast type fuel injectors) [J] . Sato Yukinori, Toh Hidemi, Watanabe Takeshi, Bulletin of GTSJ . 2002,第2002期

机译：燃烧室入口条件对燃烧室出口气体峰值温度因子的影响（通过使用带有压力雾化燃料喷嘴的燃烧室和带有鼓风型燃料喷射器的燃烧室进行的实验）
2. Influence of combustor inlet condition on combustor exit gas peak temperature factor (experiment by using the combustor with pressure atomizing fuel nozzles and the combustor with airblast type fuel injectors) [J] . Sato Yukinori, Toh Hidemi, Watanabe Takeshi, 日本ガスタ-ビン学会誌 . 2001,第1期

机译：燃烧室入口条件对燃烧室出口气体峰值温度系数的影响（通过使用带有压力雾化燃料喷嘴的燃烧室和带有鼓风型燃料喷射器的燃烧室进行的实验）
3. Influence of combustor inlet condition on combustor exit gas peak temperature factor (experiment by using the combustor with pressure atomizing fuel nozzles and the combustor with airblast type fuel injectors) [J] . Sato Yukinori, Toh Hidemi, Watanabe Takeshi, 日本ガスタ-ビン学会誌 . 2001,第1期

机译：燃烧器入口条件对燃烧器出口气峰温度因子的影响（用压力氧气喷嘴用燃烧器和空燃型燃料喷射器的试验）
4. Alternate-Fueled Combustor-Sector Performance: Part A: Combustor Performance Part B: Combustor Emissions [C] . D. T. Shouse, C. Neuroth, R. C. Hendricks, International Symposium on Transport Phenomena and Dynamics of Rotating Machinery . 2010

机译：替代燃料燃烧器 - 扇形性能：A部分：燃烧器性能第B部分：燃烧器排放
5. Optical probe for measuring the extent of air and fuel mixing in lean premixed combustors and the effect of air and fuel mixing on combustor performance. [D] . Mongia, Rajiv Kumar. 1998

机译：光学探针，用于测量稀薄预混燃烧器中空气和燃料的混合程度以及空气和燃料混合对燃烧器性能的影响。
6. Emission Reduction of Fuel-Staged Aircraft Engine Combustor Using an Additional Premixed Fuel Nozzle [O] . Takeshi Yamamoto, Kazuo Shimodaira, Seiji Yoshida, -1

机译：使用附加的预混合燃料喷嘴减少阶段式飞机发动机燃烧室的排放
7. Experimental Investigation of a Multiplex Fuel Injector Module With Discrete Jet Swirlers for Low Emission Combustors [O] . Wey, Changlie, Tacina, Robert, Mao, Chien-Pei 2004

机译：用于低排放燃烧器的带有离散射流旋流器的多重燃料喷射器模块的实验研究
8. Effect of fuel injector type on performance and emissions of reverse-flow combustor [R] . Norgren, C. T., Riddlebaugh, S. M. 1981

机译：燃油喷射器类型对逆流燃烧器性能和排放的影响

Effect of Fuel Injector Type on Performance and Emissions of Reverse-Flow Combustor

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