该产品设计用于单站泵，这些高压离心泵远程安装在发动机室。
Designed specifically for single station-systems, these high pressure centrifugal pumps mount remotely in the engine room or under the sole.
这个镜头将让游客在火箭发动机室抬头看到楼上的房间的人扭曲的看法。
This lens will let visitor to the rocket's engine room look up and see a distorted view of people in the room above.
“凯旋嘉年华”号邮轮事故调查有了新进展，今天海岸警卫队表示，致使邮轮发动机室着火并切断邮轮电力的原因是回油管路泄露。
New development in ill feet Carnival cruise liner, today the coast guard says the engine room fire that knock down power to the vessel is caused by leaking a few oil return line.
在二冲程发动机中你必须混和燃料和气体，因为气缸壁上的孔阻止使用活塞环密封燃烧室。
You have to mix oil into the gas in a two-stroke engine because the holes in the cylinder wall prevent the use of rings to seal the combustion chamber.
地点：科罗拉多州立大学发动机和能量转换实验室(EECL)？
Where: Engines and Energy Conversion Lab (EECL), Colorado State university?
汽车发动机用的化油器的组成通常包括燃油室、阻风门、怠速量孔、主量孔、空气节流喉管和加速泵。
Carburetors for automobile engines usually contained a storage chamber for liquid fuel, a choke, an idling jet, a main jet, an airflow restriction, and an accelerator pump.
很多热量从燃烧室散发出来，直接进入废弃排气系统，一部分热量进入了发动机去预热发动机。
A lot of the heat from this combustion goes right out the exhaust system, but some of it soaks into the engine, heating it up.
关于算法：图1中的数据来自于单一发动机固定条件的试验室测试结果。
Toward analgorithm: The data in Figure 1 were from a single engine underfixed test conditions in a lab.
扩散器，发动机内压气机和燃烧室间的一个部件，用来降低空气流速并增高空气压力。
DIFFUSER, a part of an engine between the compressor and combustion chamber for reducing the airflow speed and increasing the air pressure.
扩压器，发动机内压气机和燃烧室间的一个部件，用来降低空气流速并增高空气压力。
DIFFUSER, a part of an engine between the compressor and combustion chamber for reducing the airflow speed and increasing the air pressure.
针对微型燃气涡轮发动机喷嘴的雾化对燃烧室火焰稳定性、温度分布和燃烧效率的影响。
The nozzle spray characteristics of micro-turbine engines affect the stabilization of flame of the combustion chamber, the distribution of temperature, and the efficiency of combustion.
这台发动机由一个进气道，一个燃烧室和一个尾喷管组成。
This engine consists of an inlet, a combustor, and a nozzle .
对五种不同燃烧室体积的脉冲发动机在小、中和大油门开度三种供油条件下测定其排放物。
The exhaust gas ingredients of pulse engines, with five different combustion chamber volumes, throttle valve at small, middle and wide opening positions respectively, are tested.
燃烧不稳定性问题是发动机燃烧室研制过程中所遇到的难题之一，它具有极强的破坏作用。
Combustion instability, encountered in the development of researches of liquid propellant engines, is one of the significant challenges, which has tremendous destructivity.
发动机的燃烧室被凹槽围绕着。
The combustion Chambers of the engine are surrounded by pockets.
我们这里的讨论，不过，将关注更多的基本方面，这些引擎-尤其是，火箭发动机推力室。
Our discussion here, however, will be concerned with more basic aspects of those engines-in particular, the rocket engine thrust chamber.
因此，如果你的自发动机不曾频繁的在你实验室或办公桌前驻足，也许你应该帮它一把。
So if the motivation fairy hasn't been stop-ping off at your lab or desk very frequently, perhaps you should give her a hand.
在高空模拟实验器上，利用已有的航空发动机预燃室点火器，研究了燃油预热增温对高空低压点火性能的影响。
The effect of advanced fuel temperature on the high altitude ignition performance in the prechamber taken from an existent aero-engine at simulated high altitude facility was studied.
对脉冲爆震发动机的混合室进行了实验研究。
The experimental study on the mixing chamber of pulse detonation engine prototype is performed.
成功制造出带冷却通道的火箭发动机推力室身部样件。
A sample of rocket engine thrust chamber with cooling channels was successfully manufactured by APEF.
本文介绍了装载机工作装置、驾驶室、发动机罩，以及扶梯扶手、灯具及外观色彩等的造型设计。
The modeling design of the working equipment, cab, engine hood, hand rails and steps, lamps and outside colors of the loader is presented.
介绍了冲压转子发动机的工作原理，提出了适用于这种发动机的切向驻涡燃烧室新概念；
The operating principle of a ramgen is introduced, and a new concept of tangential trapped vortex combustor (TTVC) used for the engine is presented.
并根据结果分析了燃烧室压强和混合比对发动机性能的影响。
The effects of combustion chamber pressure and mixture ratio on engine performance were analyzed based on simulation.
试车结果表明，PFDH - 2绝热层可以对富氧环境下工作的发动机燃烧室实施有效热防护。
Results of subscale engine test show that the insulation (PFDH-2) can be used for heat protection of oxidizer rich solid rocket engine chamber.
采用遗传算法对某试验超燃冲压模型发动机的燃烧室构型参数进行了优化设计，所得方案的性能大大优于实际方案。
Scramjet combustor design optimization for a test scramjet model engine is conducted by employing genetic algorithms, and an optimal design much better than original design is obtained.
发动机配件类：齿轮室、气门室罩盖、链轮室罩盖、预热器座、水泵泵盖、进气歧管、泵箱；
Engine fittings series:Gear chamber, Cavaera cover, Sprocket rooms cover, Preheaterbase, Water pump Cover, Intake manifold, Pump box.
的目的，这些研究是收集数据，使他们能够适应的试验室的冲压发动机试验。
The objective of these studies is to gather data that enable them to adapt the test chamber for ramjet tests.
文中还给出了燃料总蒸发速率和单位长度上的蒸发速率随该发动机燃烧室轴向距离变化的曲线。
Curves of total vaporization rate of fuel and vaporization rate per unit length as functions of the axial distance of combustor for given rocket engine are also presented.
为了分析液体推进剂火箭发动机燃烧室中存在的非稳态环境，必须很好地了解稳态状态。
To appreciate the unsteady environment existing in liquid propellant rocket chambers it is necessary that the steady state be well understood.
为了分析液体推进剂火箭发动机燃烧室中存在的非稳态环境，必须很好地了解稳态状态。
To appreciate the unsteady environment existing in liquid propellant rocket chambers it is necessary that the steady state be well understood.
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