首页> 外文期刊>Applied thermal engineering: Design, processes, equipment, economics >Experimental study on combustion, emissions and thermal balance of high compression ratio engine fueled with liquefied methane gas
【24h】

Experimental study on combustion, emissions and thermal balance of high compression ratio engine fueled with liquefied methane gas

机译:液化甲烷气体燃料燃烧,排放和高压发动机燃烧,排放及热平衡的实验研究

获取原文
获取原文并翻译 | 示例
       

摘要

To improve the fuel efficiency of liquefied natural gas engine, an approach was proposed in our previous study, in which the liquefied natural gas is first purified into liquefied methane gas and then fueled to high compression ratio engine. To further evaluate the fuel efficiency of liquefied methane gas engine, in this study the thermal balance test was carried out, and then the thermodynamic performance of liquefied methane gas engine was analyzed and various kinds of energy losses were disintegrated. On this basis, the influence factors of various forms of energy flow in liquefied methane gas engine were discussed by combining with combustion and thermodynamics processes. Results show that, the proportions of indicated work in high-pressure cycle, exhaust energy and heat transfer loss are mainly influenced by engine speed. The high-pressure cycle efficiency increases with engine speed and the maximum value reaches 49.6% due to the higher compression ratio. The variation trend of exhaust energy proportion is similar as that of high-pressure cycle efficiency, while the proportion of heat transfer loss decreases with the engine speed increasing. Although the maximum high-pressure cycle efficiency appears in high speed conditions, the maximum effective thermal efficiency still appears at low speed due to the effect of friction loss and pumping loss (especially the former). Therefore, for the low speed conditions, the effective thermal efficiency of LMG engine can be further improved by optimizing the thermodynamic process (or combustion parameters); while for the high speed conditions, it is better to reduce the friction loss and pumping loss.
机译:为了提高液化天然气发动机的燃料效率,在我们以前的研究中提出了一种方法,其中首先将液化天然气净化成液化甲烷气体,然后燃料到高压缩比发动机。为了进一步评估液化甲烷燃气发动机的燃料效率,在该研究中进行了热平衡测试,分析了液化甲烷燃气发动机的热力学性能,并崩解了各种能量损失。在此基础上,通过与燃烧和热力学过程组合讨论了液化甲烷燃气发动机中各种形式的能量流量的影响因素。结果表明,高压循环,排气能量和传热损耗的指示工作的比例主要受发动机速度的影响。高压循环效率随发动机速度而增加,由于压缩比较高,最大值达到49.6%。排气能量比例的变化趋势与高压循环效率相似,而传热损耗的比例随发动机速度的增加而降低。尽管最高高压循环效率出现在高速条件下,但由于摩擦损失和泵送损失(特别是前者)的效果,最大有效的热效率仍然处于低速。因此,对于低速条件,通过优化热力学过程(或燃烧参数),可以进一步提高LMG发动机的有效热效率;虽然对于高速条件,但更好地降低摩擦损失和泵送损失。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号