Research on Low NO_x Combustor Using Lean Premixed Pre-Vaporized Combustion in High Temperature and High Pressure Gas Turbines

F.Toshiro; S.Tsukasa

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Research on Low NO_x Combustor Using Lean Premixed Pre-Vaporized Combustion in High Temperature and High Pressure Gas Turbines

机译：高温高压燃气轮机贫液预汽化燃烧低NO_X燃烧器研究

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Lean pre-vaporized and premixed (LPP)combustion technology was experimentally studied for thedevelopment of low NO_x gas turbine combustors operatingunder high compression ratios, such as aero-derived turbines. Toinvestigate the combustion characteristics under high-pressureand high-temperature airflow conditions of up to 3 MPa and 550deg C, a blow-down type with a regenerative heater combustiontest facility was developed. To achieve stable combustionwithout flash back and autoignition, a rapid mixing nozzle wasdeveloped. The combustion tests of the model combustor underthe above inlet condition and 1 420 deg C at the exit showed 60percent reduction of NO_x emission level compared to theconventional air-blast nozzle combustor.

机译：瘦预蒸发和预混（LPP）燃烧技术是实验研究的低NO_X燃气轮机燃烧器训练在高压缩比，例如航空衍生的涡轮机。在高达3MPa和550deg C的高压高温气流条件下致燃烧特性，开发了一种具有再生加热器燃烧器设施的排气型。为了实现稳定的燃烧速度闪回和自燃，快速混合喷嘴是展开的。与Theconventional喷嘴燃烧器相比，在出口下的上述入口条件下的模型燃烧器和1 420℃的燃烧试验显示了NO_X发射水平的60％。

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《石川島播磨技報》 |2000年第3期|共5页
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F.Toshiro; S.Tsukasa;
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中图分类机械学（机械设计基础理论）;
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1. Research on Low NO_x Combustor Using Lean Premixed Pre-Vaporized Combustion in High Temperature and High Pressure Gas Turbines [J] . F.Toshiro, S.Tsukasa 石川島播磨技報 . 2000,第3期

机译：高温高压燃气轮机稀薄预混合预燃烧低NO_x燃烧器的研究
2. Research on low NO{sub}x combustor using lean premixed pre-vaporized combustion in high temperature and high pressure gas turbines [J] . Fujimori Toshiro, Saito Tsukasa Mizutani Taku, Tou Hidemi 石川島播磨技報 . 2000,第3期

机译：高温高压燃气轮机中稀薄预混预汽化燃烧低NO {sub} x燃烧室的研究
3. Research on low NO{sub}x combustor using lean premixed pre-vaporized combustion in high temperature and high pressure gas turbines [J] . Fujimori Toshiro, Saito Tsukasa Mizutani Taku, Tou Hidemi 石川島播磨技報 . 2000,第3期

机译：使用精贫的高压燃气涡轮机使用瘦预混汽化燃烧的低NO {SUB}燃烧器的研究
4. COMBUSTION INSTABILITIES IN A LEAN PREMIXED PRE-VAPORIZED COMBUSTOR AT HIGH-PRESSURE HIGH-TEMPERATURE [C] . Xiao Han, Xin Hui, Chi Zhang, ASME turbo expo: turbine technical conference and exposition . 2017

机译：稀薄的预混合式高压燃烧器在高压高温下的燃烧不稳定性
5. Combustion instability mechanisms in a lean premixed gas turbine combustor. [D] . Lee, Hyung Ju. 2009

机译：稀薄的预混燃气轮机燃烧室中的燃烧不稳定性机理。
6. The Effect of Partial Premixing and Heat Loss on the Reacting Flow Field Prediction of a Swirl Stabilized Gas Turbine Model Combustor [O] . Simon Gövert, Daniel Mira, Jim B. W. Kok, -1

机译：部分预混合和热损失对旋流稳定型燃气轮机模型燃烧器反应流场预测的影响
7. A Case Study on Combustion Instability of a Model Lean Premixed Gas Turbine Combustor with Open Source Code OSCILOS [O] . Dong Jin Cha, Jin Kwan Song, Jong Geun Lee 2015

机译：开源代码硅料燃烧燃气燃烧器燃烧不稳定性的案例研究

Research on Low NO_x Combustor Using Lean Premixed Pre-Vaporized Combustion in High Temperature and High Pressure Gas Turbines

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