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燃烧室     
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  combustion chamber
     Judgement and Handling of Abnormal Combustion in DLN-2.0+ Combustion Chamber of 9FA Gas Turbine
     9FA燃气轮机DLN-2.0+燃烧室燃烧异常判断及处理
短句来源
     Design of the Combustion Chamber for NT6135ZR Diesel Engine
     NT6135ZR柴油机燃烧室的设计
短句来源
     Under the condition featuring a pressure of 0.5 MPa in the combustion chamber,a combustion temperature of 900 ℃,excess air ratio of 1.2 to 1.3 and fluidized speed of 1.1 to 1.2 m/s,the combustion efficiency of the semi-coke can exceed 99% with the carbon content of fly ash being below 2%.
     在燃烧室压力0.5 MPa,燃烧温度900℃,过剩空气系数1.2~1.3,流化速度1.1~1.2 m/s条件下,半焦的燃烧效率达到99%以上,飞灰含碳量在2%以下;
短句来源
     Design and Adjustment of Injection Steam System of Combustion Chamber Of S1A-02DFC Gas Turbine
     S1A-02DFC燃机燃烧室注蒸汽系统设计与调试
短句来源
     Research on CAD/CAM technology of reverse design in a combustion chamber casting core
     内燃机燃烧室芯头反求设计的CAD/CAM技术研究
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  combustor
     Moreover,combustor with L/Du=7~9,θ=30°,Du/Dd=1.0,and Ljet=24 mm is recommended regarding combustion efficiency and total pressure recovery.
     L/Du=7~9,θ=30°,Du/Dd=1.0和Ljet=24mm的燃烧室强化混合燃烧的性能较好,可以获得较高的燃烧效率和总压恢复。
短句来源
     When the flow rate of hydrogen is 3.4439 g/h and the H2/O2 ratio is 1.8, the micro-TPV system is able to deliver an electrical power output of 0.562 W in a micro combustor of 0.091 cm3 in volume.
     当H2流率为3.4439 g/h,H2/O2比为1.8时,微TPV 系统能在一个容积为0.091 cm3的微型燃烧室内产生0.562 W的电力输出。
短句来源
     The empirical model SN8 = 2.62 + 0.853was obtained from the smoking empirical model of GE F101 engine combustor.
     经验模型根据GE公司的F10 1发动机燃烧室的冒烟经验模型得出SN8=2 .6 2 +0 .85 3[ln(Ss) ]。
短句来源
     Design and Analysis of QD - 128 Aeroderivative Industrial Gas Turbine combustor
     QD-128航改燃机燃烧室设计分析
短句来源
     Cause analysis of combustor burn-through of gas turbine LM5000STIG
     LM5000STIG燃气轮机燃烧室烧穿原因分析
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  chamber
     A Study on the Mixture Formation and Air Flow in the "Bump" Combustion Chamber of A Diesel Engine
     BUMP燃烧室"内混合气形成及缸内气流运动的研究
短句来源
     AN ADJUSTING TEST OF A GAS TURBINE COMBUSTION CHAMBER USED IN A 4000 HP LOCOMOTIVE
     4000马力燃气轮机车燃烧室的调整试验
短句来源
     SOME PROBLEMS ABOUT THE METHOD OF MEASUREMENT AND CALCULATION IN THE COMBUSTION EFFICIENCY TEST OF GAS TURBINE COMBUSTION CHAMBER
     燃气轮发动机燃烧室燃烧效率试验中的测量和计算方法的某些问题
短句来源
     The Measurement of Fuel Spray of Nozzles by the Schlieren Photography and Its Compatibility with Shape of Combustion Chamber
     喷油油束的纹影测量及与燃烧室形状的配合
短句来源
     Investigation of Swirl Chamber on X105 Series Diesel Engine
     X105系列柴油机涡流室燃烧室的研究
短句来源
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  combustion chambers
     Design of Position Measuring and Milling ProcessingSystem for Combustion Chambers in G427 Engine Hood
     G427缸盖燃烧室定位测量和铣削加工系统研制
短句来源
     Numerical Studies of the Cold Flow Field in Model Combustion Chambers
     模型燃烧室冷态流场的数值研究
短句来源
     Study on the Discharge Coefficients of the Connecting Passage of the Combustion Chambers for Swirl ChamberDiesel Engines
     涡流室式柴油机燃烧室连接通道流量系数的研究
短句来源
     The performances were compared between a methanol engine, Hl495JIQ,withnew combustion chambers and with old ones.
     本文比较了改进燃烧室前后电喷甲醇HL495JIQ发动机的特性。
短句来源
     An Innovative Partition Model of Liquid Rocket Engine Combustion Chambers
     液体火箭发动机燃烧室的一种分区模型
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  combustion chamber
The operation of rocket motors is often accompanied by the development of powerful secondary vortices in the combustion chamber [1-3], The superposition of the secondary vortices on the main flow leads to the formation of a cellular flow structure.
      
The characteristics of the gas dynamic wave process taking place in a ramjet duct when the combustion chamber is started up or the fuel supply regime is switched have been investigated.
      
One-dimensional mathematical model of the combustion chamber of a hydrogen/air hypersonic ramjet
      
A mathematical model of the supersonic combustion chamber of a hydrogen/air hypersonic ramjet is proposed.
      
Other physical and chemical processes which take place in the combustion chamber, such as excitation of internal molecular degrees of freedom, hydrogen and oxygen dissociation, OH and NO formation, etc., are assumed to be equilibrium.
      
更多          
  combustor
After taking into consideration the influence of the pressure and carbon conversion ratio on the performance of the system, the gasifier and the combustor were synthetically studied.
      
A test bed was established and experimental comparisons were made between the prototype and a transferred cup atomizer micro-combustor.
      
The Possibility of Simulating in Wind Tunnels the Parameters of Hypersonic Flow and the Conditions in the Combustor of Hypersoni
      
The use of the spectral band model made it possible to construct a valid efficient algorithm for the calculation of radiation heat transfer for the conditions of a diesel combustor.
      
A theoretical investigation is performed of the emergence of acoustic vibrations under conditions of combustion of coal particles in the combustor of a pulsed MHD generator.
      
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  chamber
Weyl chamber flow on irreducible quotients of PSL(2, ?) × PSL(2, ?)
      
A seaweed-chamber experiment was performed, indicating that gaseous I2 is one of the important precursors that lead to new particle formation in the presence of solar light in the ambient air at the coastal tidal area.
      
The main process parameters studied in this work were the voltage, the flow rate of the spinning fluid, the distance between the spinneret and the nanofiber collector and the temperature in the spinning chamber.
      
It ingeniously utilizes the inner space of its chamber by developing its chamber bottom into unsymmetrical ridges along the direction of the inlet and outlet of the pump.
      
Two Y-shape pipes are fixed outside the chamber serving as an inlet and outlet, with the chamber and a piezoelectric vibrator being the actor.
      
更多          
  combustion chambers
The discrete-ordinates method is a simple, accurate and of little computational time solution to predict the radiative heat transfer in the combustion chambers.
      
For instance, impinging and multi-impinging jets atomizers are used in rocket combustion chambers, while splash-plate atomizers find their use when wall film cooling is required.
      
Pressure swirl atomizers, either of simplex or duplex kind, along with Y-Jet or Spider Jet atomizers are used in industrial applications and in turbine combustion chambers.
      
The second case characterized the reaction zone of premixed flames within gas turbine combustion chambers, based on a laboratory scale model of a lean prevaporized premixed (LPP) combustion chamber.
      
Prediction of the resonance characteristics of combustion chambers on the basis of large-eddy simulation
      
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