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车用发动机配气机构动力学及其振动特性分析
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摘要
配气机构是车用内燃机的重要组成部分,直接影响到其经济性、排放、振动噪声及可靠性。本文以洛阳北方工业集团LJ750发动机为具体的研究对象,对配气机构凸轮型线的设计,配气机构动力学以及振动情况,凸轮-挺柱副间的受力情况以及气门落座情况进行了研究。
     论文首先对国内外科研工作者在车用发动机配气机构的动力学以及振动特性研究方面的研究成果作了概述,明确了本文研究工作的重点和需要解决的主要问题。着重研究了凸轮型线的优化设计,提出了用复合形法来求解最优的凸轮型线,并讨论了凸轮型线幂指数的变化对凸轮运动特性的影响。建立了配气机构的单质量,二质量,以及多质量模型,作为研究配气机构动力学以及振动特性分析的基础。重点推导了气门弹簧的数学模型,并分析了气门刚度的变化,配气机构的转速变化以及气门间隙的变化对机构受力的影响。在动力学基础之上,分析了配气机构的振动特性,对在实际的配气机构的刚度以及弹簧刚度的选取中提出了建议。应用ANSYS/LS-DYNA软件,对气门与气门座的碰撞进行了模拟分析。
The valve train is an important part of an engine, which influences the economy, emission,NVH and reliability performance directly. Aiming at the LJ750 engine made by the Luoyang north industry group, the cam profile design, dynamics, and vibration of the valve train is researched; the force between the cam—tappet pairs and between valve–valve seat are discussed as well.
     First, the paper summarizes the research production of valve train dynamics and vibration in and out abroad, which is helpful in identifying the key problems. Secondly, special attention has been focused on the optimum design of cam profile, and approach of compound shape has been applied to the solution of optimum cam profile. Influence of the variety of power of the cam profile on the characteristics of cam movement has been discussed as well. Single mass model, two-mass model and multi-mass model of vehicle engine valve train have been established, which is the basis of analyzing dynamics and vibration of valve train. Particular attention was focused on the deduction of mathematic model of the valve spring, and the influence on the force exerted on the valve train made by the change of the valve stiffness, the change of the cam speed, and the change of the valve lash. The characteristics of the vibration are also analyzed on the biases of valve train dynamics. Suitable suggestions on the chosen of the stiffness of the valve train and the valve spring has also been put forward. Collision between valve face and valve seat has been simulated in the software environment of ANSYS/LS-DYNA.
引文
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