Journal of Jilin University(Engineering and Technology Edition) ›› 2022, Vol. 52 ›› Issue (3): 504-514.doi: 10.13229/j.cnki.jdxbgxb20200857

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Optimization on thermal load of combustion chamber on two/four⁃stroke switchable diesel engine

Yan ZHANG1(),Wei LIU1,Shu-yong ZHANG1,Yi-qiang PEI2(),Meng-meng DONG2,Jing QIN2,3   

  1. 1.National Key Laboratory of Diesel Engine Turbocharging,China North Engine Research Institute,Tianjin 300072,China
    2.State Key Laboratory of Engines,Tianjin University,Tianjin 300072,China
    3.Internal Combustion Engine Research Institute,Tianjin University,Tianjin 300072,China
  • Received:2020-11-06 Online:2022-03-01 Published:2022-03-08
  • Contact: Yi-qiang PEI E-mail:tjuzhangyan@163.com;peiyq@tju.edu.cn

Abstract:

The in-cylinder combustion process of a two/four-stroke switchable diesel engine at high load conditions under two-stroke working mode was analyzed based on the three-dimensional CFD simulation. It was found that the movement of airflow causes the mixture to burn at the edge of the piston bowl, resulting in local high temperature and local excessive thermal load. Two optimized designs of combustion chambers were obtained to adjust the match of oil and gas with chamber to improve combustion. It was found that increasing the diameter of combustion chamber expands the diffusion space of the mixture and reduces the mixture diffused above the piston bowl edge, which can avoid excessive thermal load at the piston bowl edge. Increasing the diameter of the piston pit helps produce the vortex in the pit to promote the mixture formation and shorten the combustion duration. The thermal loads of the piston bowl edge of these two designs are significantly improved, and the combustion durations of the chamber Ⅰ and chamber Ⅱ increase the power by 4.11% and 1.96% respectively. The comparison test of the original machine and chamber Ⅰ was carried out under the ablation condition of the original machine at 2800 r/min@46 kW. Compared with the original machine, the fuel consumption of the chamber Ⅰ is reduced by 6.93%, exhaust temperature is decreased by 21.1 K and the piston surface is smooth without any ablation.

Key words: power machinery and engineering, two/four-stroke switchable diesel engine, thermal load, combustion chamber design

CLC Number: 

  • TK421.2

Table1

Engine parameters"

参数数值参数数值
缸径/mm110排气门定时/°CA102/230
冲程/mm110喷油时刻/°CA347
压缩比13.3喷油量/mg83.3
进气门定时/°CA135/270

Fig.1

CONVERGE simulation model"

Fig.2

Comparison of spray penetration insimulation and experiment"

Fig.3

Comparison of in-cylinder pressure insimulation and experiment"

Fig.4

Ablation position in the experiment and istribution of heat flux in the simulation"

Fig.5

Temperature iso-surface distribution in bottom view of piston at 16 ATDC (exhaust valve side on the right)"

Fig.6

Spray development process (exhaust valve side on the left,unit:m)"

Fig.7

Equivalent ratio field and temperature field on Y-section (exhaust valve side on the left,unit:K)"

Fig.8

Equivalent ratio field and velocity field on Z-section (exhaust valve side on the left)"

Fig.9

Schematic diagram of the structural parameters of the combustion chamber"

Fig.10

Comparison of the designed combustionchamber and the prototype"

Table 2

Comparison of combustion chamberstructure parameters"

参数原机设计一设计二
燃烧室口径Dk/mm72.076.881.2
燃烧室深度H/mm14.313.312.5
凹坑直径d/mm8.920.014.9
燃烧室宽度Dl/mm75.077.283.0

Table 3

Comparison of combustion performance between the prototype and the designed combustion chamber"

参数原机设计一设计二
单循环放热/J3750.453683.353638.98
平均有效压力/MPa1.451.511.48
燃烧持续期/°CA51.4044.7046.80
有效功率/kW48.4750.4749.43
燃烧室传热/J203.94171.18182.24

Fig.11

Comparison of heat release rate"

Fig.12

Comparison of the equivalent ratio of mixture between the prototype and the designedcombustion chamber"

Fig.13

Comparison of heat flux distribution between the designed combustion chamber and the prototype"

Fig.14

Comparison of turbulent kinetic energybetween the prototype and the designedcombustion chamber (exhaust valveside on the left)"

Fig.15

Observation section"

Fig.16

Comparison of the equivalent ratio field andvelocity field of the prototype andthe designed combustion chamber"

Fig.17

Comparison of temperature distributionbetween the prototype and the designedcombustion chamber"

Fig.18

Schematic diagram of test bench"

Table 4

Comparison of parameters"

参数原机设计一
燃油消耗量/(kg·h-114.0413.13
进气温度/K322.40323.80
进气压力/kPa273.00278.10
进气流量/(kg·h-1415.00396.80
排气温度/K688.50667.40

Fig.19

Comparison of cylinder pressure betweenthe prototype and chamber Ⅰ"

Fig.20

Comparison of piston top face betweenthe prototype and chamber Ⅰ"

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