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1)  scramjet combustor
Scramjet燃烧室
1.
Three-dimensional parallel simulation of the flow-field of a scramjet combustor and comparisons with experiments;
Scramjet燃烧室流场的三维并行数值模拟及试验比较
2)  Combustion chamber
燃烧室
1.
Technology Retrofits of the Combustion Chamber in an Internal Heat Calcinator;
内热式焙烧炉燃烧室的技术改造
2.
Improvement of combustion chamber of tower-type zinc re-distillater;
韶冶塔式锌精馏炉燃烧室的改进
3.
Flux distribution of coal gas spout and air spout in combustion chamber in lead column in process of zinc refining;
锌精馏铅塔燃烧室煤气喷口和空气喷口流量分布
3)  Combustor [英][kəm'bʌstə]  [美][kəm'bʌstɚ]
燃烧室
1.
Numerical Analysis of Reaction in Combustor of DF Chemical Laser Using C_2H_2 as Fuel;
C_2H_2作燃料的DF化学激光器燃烧室反应的数值分析
2.
Rebuild on combustor of roasting kiln with concentrated H_2SO_4 for RE mineral concentrate;
包钢稀土精矿浓硫酸焙烧回转窑燃烧室的研究改造
3.
A study on NO_X formation for double swirler combustor;
双旋流器燃烧室NO_X生成研究
4)  chamber [英]['tʃeɪmbə(r)]  [美]['tʃembɚ]
燃烧室
1.
Effect of partition on ceramic burner and the flow process in the combustion chamber;
阻流板对陶瓷燃烧器及燃烧室内流动过程的影响
2.
Simulation test of high-frequency combustion instabilities of chamber with single injector;
高频燃烧不稳定性单喷注器燃烧室模拟实验的研究
3.
Principle and design of simulation test for acoustic charac-teristics of liquid rocket engine chamber with a single injector;
液体火箭发动机单喷注器燃烧室声学特性模拟实验原理及实现
5)  micro combustor
微燃烧室
1.
Micro combustor is one of the most important components in a micro-thermo-photovoltaic(MTP)system.
微燃烧室是微热光电(MTPV)系统的重要组成部分。
2.
Increasing the combustion efficiency of the micro combustor to the greatest extent is very important to the micro thermophotovoltaic systems.
最大化提高微燃烧室的燃烧效率对于微热光电系统是非常关键的。
3.
Micro combustor is one of the most important components of micro thermophotovoltaic (MTPV) system.
微燃烧室是微热光电(MTPV)系统的一个重要组成部分。
6)  Combustion chambers
燃烧室
1.
Reasonable matching between combustion chambers and helical intake port is the first to be insured in the process of matching of the three elements of combustion system on D.
直喷式柴油机燃烧系统3要素匹配时,首先应保证燃烧室和进气道的合理匹配。
2.
An innovative partition model of liquid rocket engine combustion chambers is developed in this paper,which divides combustion chambers into two regions.
发展了燃烧室的分区模型 :将燃烧室分为两个区 ,一个是燃烧区 ,采用时滞燃烧瞬时均匀混合模型 ,另一个是流动区 ,连同喷管一起 ,采用一维理想气体流动的有限元状态变量模型。
3.
Introduced is the design procedures of a multi-computer controlled loca-tion measuring and milling processing system for the combustion chambers inG427 engine hood.
介绍用多计算机控制的G427缸盖燃烧室定位测量和铣削加工系统的研制方法,并给出仿形铣削加工的算法。
补充资料:下室
1.内室;内堂。
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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