The Effects of Oil Film Shape on Piston Ring and Liner Tribology Under Mixed Lubrication

Abbas Razavykia, C. Delprete, E. Brusa, Yaser Hosseini
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引用次数: 1

Abstract

Corresponding Author: Abbas Razavykia Department of Mechanical and Aerospace Engineering, Politecnico di Torino, 10129 Torino, Italy Email: abbas.razavykia@polito.it Abstract: Mechanical power loss reduction at lubricated reciprocating and rotating components is recognized as an approach to improve the efficiency and to reduce the emissions of Internal Combustion Engines (ICEs). To achieve these goals, the instantaneous investigation of lubrication characteristics is required. Piston ring pack is of paramount importance as it is known as major contributor to frictional losses and energy dissipation. Applying Reynolds equation and lubrication theory to study piston ring tribology, requires specifying of boundary conditions. Oil film characteristics (shape and thickness) and generated hydrodynamic pressure are under influence of considered boundary conditions. Besides, the type of selected boundary conditions affects analysis robustness and sensitivity. During engine strokes, piston ring enjoys hydrodynamic and mixed lubrication regimes. The principle aim of the current study is to examine the effects of alternative boundary conditions: Half Sommerfeld, oil separation and Reynolds cavitation and reformation conditions on piston ring tribology under isothermal mixed and hydrodynamic lubrication regimes. This article demonstrates that different boundary conditions are suited to different operating conditions with respect to load, speed and temperature as well as crank angle, i.e., relative position of ring with respect to the liner. Thicker oil film thickness has been calculated applying half Sommerfeld boundary conditions under either hydrodynamic or mixed lubrication regimes followed by oil separation due to larger effective of the ring width. It was observed that considering oil separation boundary conditions results in lower deviation from experimental data, followed by Sommerfeld boundary conditions under mixed lubrication.
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混合润滑条件下油膜形状对活塞环和衬套摩擦学的影响
摘要:降低内燃机往复和旋转润滑部件的机械功率损失是提高内燃机效率和减少排放的一种途径。为了实现这些目标,需要对润滑特性进行即时调查。活塞环是至关重要的,因为它是众所周知的主要贡献者的摩擦损失和能量耗散。应用雷诺方程和润滑理论研究活塞环摩擦学,需要明确边界条件。油膜特性(形状和厚度)和产生的动水压力受到所考虑的边界条件的影响。此外,选取的边界条件的类型也会影响分析的鲁棒性和灵敏度。在发动机行程期间,活塞环享有流体动力和混合润滑制度。本研究的主要目的是研究在等温混合润滑和流体动力润滑条件下,半索默菲尔德、油分离和雷诺空化和改造条件对活塞环摩擦学的影响。本文论证了不同的边界条件适用于载荷、速度、温度以及曲柄角(即环相对于衬套的相对位置)等不同的工况。在流体动力或混合润滑条件下,由于环宽的有效性较大,油膜分离后,应用半索默菲尔德边界条件计算了较厚的油膜厚度。结果表明,考虑油分离边界条件与实验数据的偏差较小,其次是混合润滑条件下的Sommerfeld边界条件。
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