高功率密度柴油机缸盖结构对火焰传播的影响分析OA北大核心
Influences of Cylinder Head Structures on Flame Development in High Power Density Diesel Engines
探究了小缸径高功率密度柴油机缸盖结构对燃烧状态的影响,及燃烧室结构和喷油器布置对该影响的响应.基于敞口型燃烧室,采用封闭气门和补偿缸盖体积两种方式建立135 mm 缸径柴油机的仿真模型,对比其对火焰发展的影响.对阶梯型和直口型燃烧室结构的响应进行分析,并针对不同喷孔夹角和相对气门的偏角的喷油器设置进行了分析.结果显示:小缸径柴油机的缸盖凹入容积在上止点占比为 13.1%,补偿法处理造成最高燃烧压力降低 0.473 MPa,同时后燃比例加剧;不同燃烧室形状的响应主要影响火焰与缸盖的干涉,热效率最大相差 2.34%;随着喷孔夹角由 140°增大到 150°,后燃差异减小;采用相对气门非对称性的喷孔布置有利于火焰面的发展,油耗可减少 1.90 g/(kW·h).
The influence of the cylinder head structure on the combustion state of small bore diesel engines was investigated,as well as the response of chamber shape and injector arrangement to this effect.Firstly,utilizing an open-type combustion chamber,a simulation model of a 135 mm-bore diesel engine was established using closed-valve method and compensated-volume method.And the impact on flame development was compared.The response of stepped and straight combustion chamber shapes was analyzed.Injector settings with different nozzle angles and relative valve declination angles were examined.The results show that the recessed volume of the cylinder head of the small-bore diesel engine accounts for 13.1%at top dead center.With the utilization of the compensated-volume method the peak pressure decreases by 0.473 MPa,and the proportion of post-combustion is exacerbated.The response of different chamber shapes primarily affects the interference between the flame and the cylinder head,resulting in a maximum difference in thermal efficiency of 2.34%.Furthermore,as the nozzle angle increases from 140° to 150°,the difference in post-combustion decreases.Additionally,the asymmetrical arrangement of the nozzle with valves promotes the development of the flame surface,leading to a reduction in fuel consumption by 1.90 g/(kW·h).
王鑫浩;牛晓晓;刘龙;王洋
哈尔滨工程大学 动力与能源工程学院,哈尔滨 150001河南柴油机重工有限责任公司,洛阳 471003哈尔滨工程大学 动力与能源工程学院,哈尔滨 150001哈尔滨工程大学 动力与能源工程学院,哈尔滨 150001
能源与动力
高功率密度柴油机缸盖结构燃烧室形状喷孔夹角喷孔偏角
high power density diesel enginecylinder head structurechamber shapenozzle anglenozzle deflection angle
《内燃机工程》 2025 (1)
27-35,9
国家自然科学基金项目(U2241262)National Natural Science Foundation of China(U2241262)
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