除了凹面镜，能量塔以外，还有第三种新的太阳能热技术。结合了曲线，盘状镜面和热发动机的装置。
In addition to parabolic troughs and power-towers there is also a third solar-thermal technology, which combines curved, dish-shaped mirrors with heat engines.
在这一点上残留或灰尘微粒的控制，以建立或不重视热发动机部件或建立在石油以来的粒子悬浮在油。
At this point residue or dirt particles are controlled to not build up or attach to hot engine parts or build up in the oil since the particles are suspended inside the oil.
专有的斯特林发动机能有效地太阳能或废热转换成电能。
The proprietary Stirling engine was developed by Cool energy to efficiently convert solar thermal energy or waste heat into electricity.
Blue - NG，一家开发英国项目的合资公司，打算使用搭配涡轮放大器的同时，搭配上能产生电和热的热电联产发动机，从而达到削减成本的目的。
Blue-NG, the joint venture developing the UK projects, aims to reduce costs by combining the turboexpander with a combined heat and power (CHP) engine, which generates both electricity and heat.
在这种发动机中，空气通过燃烧燃料转换成高速运动的一阵热的气体。
In this engine, air is converted, by burning fuel, into a blast of hot gas moving at high velocity.
不像纽科门的发动机，瓦特设计了一个冷凝器，可以酷，而缸热。
Unlike Newcomen's engine, Watt's design had a condenser that could be cool while the cylinder was hot.
有人会问：如今的发动机技术比以前领先，还有必要这么考究热车吗？
Some people will ask: now the engine technology than the previous leader, and so elegant is necessary?
当机油经过发动机的热的部件时，它将带走一定量的热量。
As the lubricating oil passes over a hot engine part, it removes a certain amount of heat.
对某车型发动机排气歧管的热疲劳断裂问题进行综合失效分析，并从材料、结构方面提出改进意见。
This paper gives a comprehensive failure analysis on the thermal fatigue crack of engine exhaust manifold and makes an improvement for materials and structures.
热扰动是由安装在发动机进口前的氢燃烧温度畸变发生器产生的。
A temperature distortion generator burning hydrogen in front of engine inlet produces thermal disturbance.
活塞的热疲劳性能对柴油发动机的全寿命至关重要。
Thermal fatigue behavior of the piston is vital to the overall life-span of diesel engines.
不同室外温度下的燃气机热泵热负荷、供热量、发动机的余热量、系统一次能耗的变化关系。
Different outdoor temperature of the gas engine heat pump under the heat load for the heat, heat the remainder of the engine, the system changes in a power relationship.
节温器非线性动态特性与发动机热系统延迟效应相互作用，使系统动态特性复杂。
The interplay between thermostat nonlinear dynamic characteristics and engine thermal system hysteresis complicates system transient phenomena.
计算结果可为级间分离段和发动机热防护的设计提供参考。
This can provide basis for the design of the stage separation part for a rocket and the thermal protection of the engine.
根据物理上直观的拉格朗日法，分析了交变流动发动机中回热器内代表性气体微团的热力过程和循环。
The thermodynamic processes and cycles of some characteristic gas parcels in the regenerator in a cyclic flow engine are analyzed thoroughly in Lagrangian's view.
某些制造厂商反对在发动机处于热态以及冷却系内压力依然较高时打开水箱盖。
Some manufacturers warn against taking off the cap when the engine is hot and pressure in the cooling system is high.
提出了航空发动机防喘控制系统设计和研制方法，分析了当战斗机发射导弹时热扰动参数对发动机的影响。
The design and development methods of aeroengine anti-surge control system are presented. Effects of heat disturbance parameters on the engine are analyzed during missile launch.
增压发动机热负荷的增加会影响发动机的使用寿命。
Thermal load increase has influence on service life of supercharged engines.
斯特林冷却器必须拒绝的两倍多热的奥托或柴油发动机散热器。
Stirling cooler must reject twice as much heat as an Otto - or Diesel-engine radiator.
用有限元素法数值模拟了固体火箭发动机喷管内缝隙的流场和热环境。
The flow field and thermal environment of gap in solid rocket nozzle were simulated by finite element method.
试验结果还表明，热面点火系统的设计对发动机性能有着极为重要的影响。
The experimental results also show that the design of the hot-surface ignition system is of parparamount importance to the engine performance.
进行三个脉冲管与行波型热声发动机的配合实验，着重研究了热端气体温度、冷端温降和压力振幅的变化规律。
The experiment focuses on the temperature of the gas in the hot end heat exchanger, the temperature decline of the cold end of the pulse tube and pressure amplitude.
由于发动机内工作过程非常复杂、影响因素众多，对发动机内传热及热负荷的研究目前主要还是采用实验测试的方法。
Because the inside work processing of engine is very complex, and the influence factor are numerous, the heat transfer and thermal load inside engine are primarily investigated by means of experiment.
单组元肼分解发动机的热控制与热分析是空间推进系统重要组成部分。
Thermal control of monopropellant catalytic decomposition hydrazine engines in important portion of space propulsive system.
再生冷却技术是超燃冲压发动机燃烧室热防护的关键技术。
Regenerative cooling technology is one of the key technologies to thermally protect scramjet chamber.
为了充分发挥热声发动机可利用低品位热能的优势，进一步降低系统的起振温度对热声热机的应用具有重要意义。
In order to take full use of energy of low quality, further decreasing onset - temperature of thermoacoustic engines may be an effective approach.
以热力学第一定律为基础，引入多孔介质换热模型，建立了多孔介质发动机的能量方程。
An energy equation that incorporates a heat transfer model of porous medium is developed based on the first thermodynamic law.
热声发动机利用热声效应把热能转化为声功，系统中不存在任何机械运动部件。
A thermoacoustic engine converts thermal energy into acoustic power by thermoacoustic effect without any mechanical moving parts.
为提高热声发动机的热力性能，采用氦-氩混合工质对一台驻波型热声发动机进行了无负荷工况的试验研究。
To enhance the performance of a thermoacoustic prime mover, a series of experiments were conducted by using He-Ar mixture as working fluid.
为提高热声发动机的热力性能，采用氦-氩混合工质对一台驻波型热声发动机进行了无负荷工况的试验研究。
To enhance the performance of a thermoacoustic prime mover, a series of experiments were conducted by using He-Ar mixture as working fluid.
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