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1)  large velocity difference jet combustor
大速差射流燃烧室
2)  TJ Jet combustion chamber
射流燃烧室
1.
On the basis of the measured indicator diagram and NO x emission of a single cylinder gasoline engine with TJ Jet combustion chamber,a new improved multi zone combustion diagnostic model is used to get the heat release rate,the average temperature of burned gas and NO x formation rate as well as other important parameters.
对采用射流燃烧室的新型高压缩比稀混合气 492 QS车用汽油机 ,在单缸机实测示功图和 NOx 排放数据基础上 ,结合由新改进的多区燃烧分析模型经计算得到的燃烧放热率、已燃气体平均温度、NOx生成率等有关结果 ,分析了燃烧特性与 NOx 生成特性之间的关系。
2.
This paper describes an investigation on the applications of TJ Jet combustion chamber in the vehicle gasoline engines.
本文介绍了射流燃烧室在车用汽油机上的应用研究。
3)  large-velocitydifference-jet recirculating flow
大速差射流回流
4)  Jet combustion
射流燃烧
1.
According to the current popular Non Uniform Rational B spline (NURBS) principles in the international CAD/CAM field, this paper studies the surface modelling and fitting of the tube of Jet combustion gasoline engine cylinderhead.
本文以当前国际上CAD/CAM领域最流行的非均匀有理B样条(NURBS)理论为数学模型,对射流燃烧汽油机缸盖模具的气道进行了曲面造型和曲面拟合;并结合气道曲面的实际,在数控加工中对气道曲面通过轴心线实施了分段剖分,并采用参数线法确定了刀心轨迹,进行刀具轨迹仿真,获得了数控加工气道曲面和型芯的NC程序。
5)  swirl combustor
旋流燃烧室
1.
A test facility for swirl combustor with coaxial jets and staged air injection was designed, fabricated, and set up.
建立了采用分级进风方式的同轴射流旋流燃烧室实验装置,选用耐高温的氧化铝细粉作为示踪粒子,实现了用三维激光粒子动态分析仪(PDA)测量湍流旋流燃烧的热态瞬时速度场。
2.
For the purpose of developing swirl combustors with high combustion efficiency and low pollutant emission, a numerical simulation of swirling turbulent flows in a swirl combustor with coaxial jet interactions is performed.
针对发展高效低污染旋流燃烧技术的需要 ,对旋流燃烧室内两股同轴旋转射流相互作用的湍流旋流流动进行了数值模拟 。
3.
A presumed probability density function(PDF) model for temperature fluctuation is proposed and formulated in this paper to simulate propane turbulent four-step reaction,which model is employed to numerically simulate propane turbulent combustion in a swirl combustor.
应用该模型对旋流燃烧室内的丙烷湍流燃烧进行了数值模拟。
6)  reverse flow combustor
回流燃烧室
1.
Numerical simulations of two-phase reacting flow in an annular reverse flow combustor were developed in a three-dimensional non-orthogonal curvilinear coordinate system.
在三维任意曲线坐标系下数值模拟回流燃烧室火焰筒内两相燃烧过程,采用RNGk-ε模型模拟紊流粘性、EBU-Arrhenius模型模拟燃烧反应速率、离散坐标模型以及六通量模型考虑辐射传热,液相采用颗粒轨道模型,气相采用SIMPLE算法求解,并用PSIC算法考虑气液两相之间的相互作用的影响,计算得到燃烧室内速度、温度等各气流参数分布。
补充资料:五大虚空藏菩萨速疾大神验秘密式经
【五大虚空藏菩萨速疾大神验秘密式经】
 (经名)一卷,唐金刚智译。说五大虚空藏修法之仪轨。
说明:补充资料仅用于学习参考,请勿用于其它任何用途。
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