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Preliminary tests of a gas turbine combustor with an air atomizing fuel injector system

机译：燃气轮机燃烧室与空气雾化燃料喷射系统的初步试验

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Feasibility and performance of air atomizing fuel injector in turbojet combustor

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作者
Bigelow, J. A.;
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年度 1969
页码 1-16
总页数 16
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AIR; ATOMIZERS; COMBUSTION CHAMBERS; FUEL INJECTION; PERFORMANCE TESTS; TURBOJET ENGINES; FEASIBILITY; FUEL SYSTEMS; SPRAY NOZZLES;

机译：空气;雾化器;燃烧室;燃油喷射;性能测试;涡轮发动机;可行性;燃油系统;喷雾喷嘴;

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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. FLOW IN ATOMIZERS: INFLUENCE OF DIFFERENT PARAMETERS ON THE PERFORMANCE CHARACTERISTICS OF PLAIN ORIFICE ATOMIZER AND PRESSURE SWIRL ATOMIZER OF A FUEL INJECTION SYSTEM OF GAS TURBINE COMBUSTOR [C] . Digvijay B Kulshreshtha, S A Channiwala ASME(American Society of Mechanical Engineers) Fluids Engineering Division Summer Conference(FEDSM2005) vol.1 pt.B; 20050619-23; Houston,TX(US) . 2005

机译：原子流量：不同参数对燃气轮机燃烧器燃料喷射系统的平原有机物雾化器和旋流式雾化器性能的影响
5. Design and construction of a gas turbine combustor test rig for alternative fuel testing. [D] . Murphy, Crystal Marie. 2004

机译：用于替代燃料测试的燃气轮机燃烧器测试台的设计和建造。
6. Preliminary Investigations of an Opposed Rotary PistonCompressor for the Air Feeding of a Polymer Electrolyte Membrane FuelCell System [O] . Shikai Xing, Jianbing Gao, *, 2020

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7. Optical Fuel Injector Patternation Measurements in Advanced Liquid-Fueled, High Pressure, Gas Turbine Combustors [O] . Locke R. J., Hicks Y. R., Zaller M. M., 1998

机译：先进的液体燃料，高压，燃气轮机燃烧器中的光学燃料喷射器图案测量

Preliminary tests of a gas turbine combustor with an air atomizing fuel injector system

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