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Simulation and Test Research for Integrated Exhaust Manifold and Hot End Durability

机译:集成排气歧管和热端耐久性的仿真与试验研究

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In order to reduce emissions, size and manufacturing cost, integrated exhaust manifold become popular in gasoline engine, especially in three-cylinder engine. Moreover, due to shorter length, lighter weight, and less component connections, the exhaust manifold and hot end durability will improve apparently. In this work, an advanced cylinder head with integrated exhaust manifold is adopted in a three-cylinder turbo engine. Because of this integration characteristic, the gas retain in cylinder head longer and the temperature reach higher level than normal cylinder head, which will cause thermal fatigue failure more easily. To validate the exhaust manifold and hot end durability, series simulation and test validation work have been done. Firstly, overall steady state and transient temperature simulation was done for global model. For turbocharger, in order to simulate the outlet turbulent flow and 3d rotation, a code was compiled to define this 3d rotation. In this code, the inlet boundary was defined by turbine blade’s rotational velocity, direction and angle. Secondly, based on temperature prediction, thermal modal, high cycle fatigue (HCF) and thermal mechanical fatigue (TMF) analysis were done in sequence. According to HCF analysis, catalyst bracket fatigue factors fulfilled the require limit. According to TMF analysis, cylinder head life which contains the exhaust manifold fulfilled the life cycle target. Temperature and vibration test were done on rig test, good correlation is shown between test and simulation results. Finally, no crack failure was found inside the cylinder head and hot end after durability test, which also proved the TMF and HCF results indirectly.
机译:为了减少排放,尺寸和制造成本,综合排气歧管在汽油发动机中流行,特别是在三缸发动机中。此外,由于长度较短,重量较轻,而且元件连接较少,排气歧管和热端耐久性显然会改善。在这项工作中,三缸涡轮发动机采用具有集成排气歧管的先进气缸盖。由于这种整合特性,气体保持圆柱体较长,温度达到比正常气缸盖更高的水平,这将更容易地引起热疲劳失效。为了验证排气歧管和热端耐用,已完成系列仿真和测试验证工作。首先,为全球模型进行总体稳态和瞬态温度模拟。对于涡轮增压器,为了模拟出口湍流和3D旋转,编译了代码以定义该3D旋转。在该代码中,入口边界由涡轮叶片的旋转速度,方向和角度限定。其次,基于温度预测,序列完成热模态,高循环疲劳(HCF)和热机械疲劳(TMF)分析。根据HCF分析,催化剂支架疲劳因子满足需要限制。根据TMF分析,圆柱体寿命,其中包含排气歧管的实现终身目标。在钻机测试上进行温度和振动试验,在测试和仿真结果之间显示了良好的相关性。最后,在耐久性测试后,在气缸盖和热端内没有发现裂缝失效,这也被间接证明了TMF和HCF结果。

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