燃烧室

燃料喷进燃烧室

Fuel gushes into the combustion chamber .

CCD计测量燃烧室截面温度场的原理研究

Theoretical Study on Measurement of Cross Section Temperature Distribution in Combustion Chamber with CCD Camera

带多圈环形V型稳定器的加力燃烧室两态燃油浓度分布计算

Calculation of fuel concentration distribution in afterburner with V-shape flameholders

认识到建立固体火箭发动机燃烧室X射线探伤像质计标准势在必行。

It was considered that the establishment of radiographic IQI standard for solid rocket motor chamber was necessary .

本文针对W火焰煤粉燃烧室进行了全数值模拟。

In this article , the systematic numerical simulations were conducted for W-shape flame boiler furnace .

航空燃气涡轮发动机燃烧室的NOx控制及预测

Control and Prediction of NOx Formation in Aircraft Gas Turbine Engine Combustor

低NOx排放微型燃气轮机燃烧室的数值模拟及实验研究

Numerical and Experimental Investigation on a Low NOx Emission Combustor for Micro Gas Turbine

城市生活垃圾焚烧炉燃烧室三维辐射传热的Monte-Carlo解法

Three-dimensional Monte-Carlo Modeling of Radiative Transfer in a Municipal Solid Waste Incinerator

本文采用仿真技术和模拟试验的方法对可变燃烧室（VCC：VariableCombustionChamber）活塞的动力学特性进行了研究。

Using dynamical simulation in combination with analogue test , the dynamical characteristics of VCC ( Variable Combustion Chamber ) piston are studied .

TDI造气工段燃烧室设计

The Design of the Combustion Chamber for TDI Gas-making Workshop Section

应用PDA研究ω燃烧室的气缸内紊流场

Investigation on Turbulent Flow Fluid inside Cylinder for Two Types of ω Combustion Chamber Using PDA

气体燃料组分变化对SG2-6A燃气轮机燃烧室性能的影响

Effects of alternative fuel components on performances of a gas turbine combustor

MHD燃煤燃烧室的研究、分析与展望

Studies , Analysis and Prospects for Coal-Fired MHD Combustors

Scramjet燃烧室流场的三维并行数值模拟及试验比较

Three-dimensional parallel simulation of the flow-field of a scramjet combustor and comparisons with experiments

用RTR技术确定SRM燃烧室凝相粒子加入边界条件

Determination of injection boundry condition of particles in SRM chamber based on RTR techniques

全尺寸燃烧室的实验结果表明，空气加湿对于碳氢燃料与合成气火焰污染物排放的影响不同，尤其是对CO排放的影响。

The experimental results of a full-size combustor show that the influence of humid air on pollutant emission is different for hydro-carbon fuels and synthesis gas , especially on CO emission .

LRE模型燃烧室燃烧过程数值模拟

Numerical simulation of combustion process in LRE test combustion chamber

用LDV研究柴油机不同燃烧室对缸内湍流场的影响

Investigation on Effects of Different Piston-Bowl Structures on In-Cylinder Turbulent Flow Field of Diesel Engine by LDV

重点介绍了EFE型发动机的风扇加力燃烧室、喷管系统设计改进的特点。

Design improvement characteristics of EFE fan afterburner and nozzle system are particularly discussed .

模拟结果表明Realizablek–模型为最适合燃烧室数值计算的湍流模型。

Simulation results show that the Realizable k - ε model and the experimental results are close and is the most appropriate of the turbulent models for the combustion numerical calculation .

由Ni－Cr合金制成的燃烧室壁，在烃燃料燃烧的气氛中产生金属外逸型坑点状破坏，严重时可烧穿。

The burning chamber made of Ni-Cr alloy , can be destroyed under the incompletely burning condition of hydrocarbon fuel . The wall of the burning chamber was pitted at the beginning then gradually burnt through .

结果表明MMT经过燃烧室燃烧反应，主要生成固态含锰的无机盐，其以锰的磷酸盐、硫化物、硫酸盐和氧化物四类为主。

The results indicated that the MMT 's combustion products are maked up of solid inorganic compounds , such as Mn-oxide , Mn-sulfate , Mn-sulflde and Mn-phosphate .

通过求解广义一维非定常Euler方程，数值模拟了氢燃料的燃烧室，并和实验结果进行了比较和分析。

First , hydrogen-air scramjet combustor is numerically simulated and analyzed by solving the general one-dimensional unsteady Euler equation . Second , compressible , reacting , turbulent flow solutions are obtained .

主要探讨了AP含量、Mg/Al比例、HTPB粘合剂含量、燃烧室压强对凝聚相C、Mg、Al燃烧产物含量的影响。

The influences of AP content , Mg / Al ratio , HTPB binder content , pressure of combustion chamber on the content of condensed phase C , Mg , Al in combustion products were discussed mainly .

试验结果表明，与使用EPDM绝热层材料相比，使用RTV绝热层材料，火箭发动机燃烧室羽流具有较高的信号透过率；

The test results show that the plume from the rocket chamber using RTV insulation material has higher signature penetrating rate than that using EPDM insulation material .

通过对铅塔燃烧室进行测试，并经过测试和计算，结果表明：铅塔燃烧室内存在上三角高温燃烧区以及下三角燃烧低温区，同时，高温烟气中含有不同含量的可燃物CO；

The results from the measurement of combustion chamber in the lead column reveal that there are high temperature combustion in upper triangle region and low temperature combustion in lower triangle region and there is different content combustible CO in high temperature smoke .

燃气再循环（CGR）技术成功解决了热气机燃烧室的高压燃烧问题。

The technology of Combustion Gases Recirculation ( CGR ) has successfully solved the problem of high-pressure combustion of Stirling engine .

由新设计的涡流室镶块所构成的球锥形平底涡流室称QZ型涡流室式燃烧室。

The sphere-cone-flat bottom swirl chamber made of new designed swirl chamber insert is called the QZ-type swirl chamber .

本文介绍近年轿车柴油机在电子控制、燃烧室、多气门、EGR、增压、喷油和废气后处理方面的发展趋势。

The developing trend of electronic control , combustion chamber , multivalve , EGR , turbo , injection and emission after treatment etc. in diesel car is introduced in this paper .

用RTR技术研究固体火箭发动机燃烧室中粒子运动轨迹（I）可行性分析与试验研究

Experimental study of particles trajectory in firing solid rocket motor with RTR TECHNIQUE part ( I ) analysis of feasibility and experimental results