内燃机缸套空化研究中动态条件下缸套速度计算

IF 1.1 Q3 TRANSPORTATION SCIENCE & TECHNOLOGY
Sanjib Chowdhury
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引用次数: 0

摘要

针对由活塞、连杆、曲柄销和衬套组成的单缸内燃机,提出了一种非线性三维多体动态时域分析方法。这个活塞被建模为一个三维活塞,与一个真正的发动机的衬垫碰撞。目的是研究活塞拍打力和随后的衬垫振动。衬管振动速度直接导致冷却剂区域的压力波动,从而导致气泡的形成和随后的崩溃。如果气泡破裂距离尾管表面较近,则可能发生尾管的空化侵蚀。对尾管空化的机理进行了简要的解释,需要一个完整的计算流体力学(CFD)模型来展开,这超出了本工作的范围。然而,作为第一步,本方法侧重于全面准确地估计最高向内和向外的线速度,它们分别与气泡的形成和破裂直接相关。确定了衬管速度对不同发动机工作条件(温暖和炎热,裙边最高温度为178°C和130°C)、活塞销孔偏移量(推力侧、反推力侧方向的偏移量为0.6 mm,标称无偏移情况)和衬管厚度的敏感性。热工况下活塞裙套与衬套之间存在干涉现象,热工况下活塞裙套与衬套之间存在最小间隙。提出了发动机尾管空化侵蚀与尾管速度等值线图的关系。分析模型显示,在额定发动机运行配置下,无活塞销偏置的最大衬套向内速度为55毫米/秒。在最高尾管速度的位置与现场实际空化侵蚀的位置之间发现了相关性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Cylinder Liner Velocity Calculation under Dynamic Condition in the Pursuit of Liner Cavitation Investigation of an Internal Combustion Engine
An analytical method for nonlinear three-dimensional (3D) multi-body flexible dynamic time-domain analysis for a single-cylinder internal combustion (IC) engine consisting of piston, connecting rod, crank pin, and liner is developed. This piston is modeled as a 3D piston that collides with the liner as in a real engine. The goal is to investigate the piston slap force and subsequent liner vibration. Liner vibrational velocity is directly responsible for pressure fluctuations in the coolant region resulting in bubble formation and subsequent collapse. If the bubble collapse is closer to the liner surface, cavitation erosion in the liner might occur. The mechanism of liner cavitation is briefly explained, which would take a full computational fluid dynamics (CFD) model to develop, which is out of scope for the present work. However, as a first step, the present method focused on a comprehensive and accurate estimation of the highest inward and outward liner velocities, which are directly related to the bubble formation and collapse, respectively. Sensitivity of liner velocity to different engine-operating conditions (warm and hot, with highest skirt temperatures of 178 and 130°C), piston pin bore offsets (thrust side, anti-thrust side directions in the amounts of 0.6 mm, and the nominal no offset case), and liner thicknesses are determined. Piston thermal growth is considered as part of the analysis resulting in interference condition between piston skirt and liner under the hot operating condition and low minimum clearance under the warm condition. Correlation of liner velocity contour plots with real engine liner cavitation erosion is presented. Analytical model showed a maximum liner inward velocity of 55 mm/s with no piston pin offset under nominal engine-operating configuration. A correlation has been found between location of this highest liner velocity and location of the actual cavitation erosion in the field.
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来源期刊
SAE International Journal of Engines
SAE International Journal of Engines TRANSPORTATION SCIENCE & TECHNOLOGY-
CiteScore
2.70
自引率
8.30%
发文量
38
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