1) hydrogen engine
氢发动机
1.
Model Practice of Optimized Performances of Hydrogen Engine by Controlled Excess Air Ratio;
最佳过量空气系数优化控制氢发动机性能的建模实现
2.
The Combustion Characteristic and Performance Analysis of Hydrogen Engine Based on AVL-BOOST;
基于AVL-BOOST的氢发动机燃烧特性和性能分析
3.
In order to analyze and study the operation characteristic of the hydrogen engine,predicting the impact on performance when many kinds of parameters change,zero-imension model of linking to the combustion process of the hydrogen engine is applied,carring on the numerical simulation.
为了分析和研究氢发动机的运行特性,预测多种参数变化对性能的影响,对氢发动的燃烧过程建立零维模型,进行数值模拟。
2) hydrogen-fueled engine
氢发动机
1.
The pressure signals of hydrogen-fueled engines contain abundant combustion information that can be extracted by wavelet transform.
氢发动机燃烧压力信号包含了丰富的燃烧信息,基于压力信号可以应用小波变换法提取异常燃烧信息。
2.
Then,the research on exhaust characteristics of hydrogen-fueled engine under high-pressure injection with different ignition timing and injection timing was also implemented.
研究了在汽油中加入氢气后混合燃料发动机的排放特性,给出了氢汽油混合燃料可以全面改善汽油机的废气排放,然后进行了高压喷射型氢发动机的两个主要运转参数(点火提前角和喷氢提前角)对NOx排放影响的研究。
3.
The performances of a hydrogen-fueled engine with intake manifold in jection in various ignition times were carried out.
进行了进气管喷射的氢发动机点火提前角对发动机性能影响的研究,试验指出了点火提前角对氢发动机动力性,经济性和排放性能有较大影响。
3) hydrogen fueled engine
氢发动机
1.
The Design of Hydrogen Injection Control Algorithm on Hydrogen Fueled Engines;
氢发动机喷氢控制算法设计
4) hydrogen fueled internal combustion engine
氢燃发动机
1.
The advantages and main problems of hydrogen fueled internal combustion engine are introduced.
介绍了氢燃发动机的优势和现阶段氢燃发动机存在的主要问题、国内外对解决或减轻这些问题的方法及其机理。
5) hydrogen engine
氢气发动机
1.
Analysis on the situation and development of hydrogen engines;
氢气发动机的现状及前景分析
6) Hydrogen oxygen engine
氢氧发动机
1.
Following a brief analysis of the characteristics of several kinds of power cycles,the discussion is emphasized on the cryogenic technique of the high pressure closed cycle hydrogen oxygen engine.
简要分析几种不同动力循环的特点， 重点介绍大推力、高性能氢氧发动机采用补燃动力循环进行的研究及高压补燃氢氧发动机中的低温技
补充资料：航空发动机推重比(见航空发动机推力)
航空发动机推重比(见航空发动机推力)
thrust to weight ratio of aeroengine
hQngkong角dong)1 tuizhongbi航空发动机推重比〔thros*:。wdgh:ra-tio of aeroengine)见航空发动机推力。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条