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Lean Premixed Prevaporized (LPP) Gas Turbine Combustor Measurements of Flame Locations and Shear Layer Properties

机译:精益预混液化(LPP)燃气轮机燃烧器燃烧器燃烧器火焰位置和剪切层性能

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A Lean Premixed, Pre-vaporized (LPP) gas turbine combustor is studied in order to quantify the flame location and the strength of vortices that are shed in the shear layers. LPP combustors are known to provide reduced levels of nitric oxides, but they can experience unwanted pressure oscillations at off-design conditions. Three key governing mechanisms are: the relative locations of the Main and Pilot flames, the strength of the shed vortices in the shear layers, and the oscillations of the central recirculation zone. Flame location is important because it affects the uniformity of the temperature field , which leads to low NOx, and it determines how the heat release couples with the pressure field. Flame location also governs how the main flame is anchored by the pilot flame; improved flame anchoring can remove one of the sources of combustion instabilities. Previous LPP studies have primarily been limited to gaseous fuels, atmospheric pressure, and unrealistically simple injector geometries having only one flame. In this study a simple cylindrical combustor geometry is used, but a realistic LPP fuel injector is operated which provides a central nonpremixed Pilot flame that interacts with an outer premixed Main flame. Liquid Jet-A fuel is burned at elevated pressures and preheated air temperatures. Methods were developed to apply formaldehyde PLIF to visualize flames in this harsh environment. The following parameters were selected for measurement because they are good choices to use to assess the ability of LES codes to simulate the unsteady dynamics. a) Profile of flame surface density b) Profiles of flame brush thickness c) PDF of flame length, including its mean and variance d) PDF of strength of vortices shed in the primary shear layer, including their means and variances e) PDF of the size of the recirculation zone, including its mean and variance f) Profiles of Reynolds stresses and turbulence levels.
机译:研究了精益预混的预混合(LPP)燃气轮机燃烧器,以定量剪切层中脱落的火焰位置和涡流的强度。已知LPP燃烧器提供减少的一氧化氮水平,但它们可以在非设计条件下体验不需要的压力振荡。三个关键的控制机制是:​​主要和先导火焰的相对位置,剪切层中的棚涡流的强度,以及中央再循环区的振荡。火焰位置很重要,因为它会影响温度场的均匀性,这导致低NOx,并且它决定了热释放的耦合如何与压力场耦合。火焰位置也管理主火焰的锚固火焰;改进的火焰锚固可以去除燃烧不稳定性的一个。以前的LPP研究主要限于气态燃料,大气压和不切实际的简单的注射器几何形状,只有一火焰。在该研究中,使用简单的圆柱形燃烧室几何形状,但是操作现实的LPP燃料喷射器,其提供一种与外部预混的主火焰相互作用的中央非增速导频火焰。液体射流 - 燃料在升高的压力下燃烧并预热空气温度。开发了方法以将甲醛PLIF应用于这种恶劣环境中的火焰。选择以下参数进行测量,因为它们是用于评估LES码模拟不稳定动态的能力的良好选择。 a)突起的曲线表面密度b)火焰刷厚度的曲线c)火焰长度的PDF,包括其平均值和方差d)PDF在初级剪切层中的涡流强度的PDF,包括它们的手段和差异e)PDF再循环区的大小,包括其平均值和方差f)雷诺应力和湍流水平的曲线。

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