Optimizing Load Capacity Predictions in Gas Foil Thrust Bearings: A Novel Full-Ramp Model

IF 3.1 3区 工程技术 Q2 ENGINEERING, MECHANICAL
Ming Ying, Xinghua Liu, Yue Zhang, Chongbing Zhang
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Abstract

Gas film thickness significantly influences the performance prediction of Gas Foil Thrust Bearings (GFTB). However, the Classical Model (CM) for GFTBs exhibits inaccuracies in describing gas film thickness. In this paper, we explore the differences in the details of gas film thickness modeling and propose a Parallel Segmentation Model (PSM), which fixes the errors of the CM in describing the gas film thickness in the ramp section, and a Full-Ramp Model (FRM), to which a more realistic description of the gas film in the flat section is also added. Comparative analysis, utilizing a publicly available test dataset based on the open-source GFTB structure, establishes that the FRM surpasses the CM and PSM in accurately predicting load capacity. In-depth analysis shows that the location of the minimum gas film thickness for determining the load capacity is located at the innermost circle of the free end of the top foil, whereas the FRM is subjected to the same load with a larger film thickness at this location, which may be due to the unique geometry of the top foil of the FRM. Subsequently, employing the FRM, a parametric study explores load capacity in GFTB, considering variables such as ramp height, top foil thickness, bump foil stiffness, ramp section extent, and top foil area. The results demonstrate that GFTB load capacity exhibits a linear increase with the expansion of the top foil area. Moreover, the load capacity increases with augmented top foil thickness and bump foil stiffness, albeit at a decreasing rate. Additionally, an increase in ramp section extent initially enhances load capacity, reaching a maximum value before declining. Similarly, an increase in ramp height initially augments load capacity, attaining a maximum before subsequent diminution.
优化气体箔推力轴承的负载能力预测:新型全斜坡模型
气膜厚度对气膜推力轴承(GFTB)的性能预测有很大影响。然而,用于 GFTB 的经典模型(CM)在描述气膜厚度时存在误差。本文探讨了气膜厚度建模细节上的差异,并提出了平行分段模型(PSM)和全斜面模型(FRM),前者修正了 CM 在描述斜面部分气膜厚度时的误差,后者则增加了对平面部分气膜更真实的描述。利用基于开源 GFTB 结构的公开测试数据集进行的比较分析表明,FRM 在准确预测负载能力方面超过了 CM 和 PSM。深入分析表明,确定负载能力的最小气膜厚度位置位于顶箔自由端最内圈,而 FRM 在承受相同负载时,该位置的气膜厚度更大,这可能是 FRM 顶箔的独特几何形状造成的。随后,考虑到坡道高度、顶箔厚度、凸起箔刚度、坡道截面范围和顶箔面积等变量,利用 FRM 对 GFTB 的负载能力进行了参数研究。结果表明,随着顶箔面积的扩大,GFTB 的承载能力呈线性增长。此外,承载能力随着顶箔厚度和凸块刚度的增加而增加,尽管增加的速度在减小。此外,坡道截面范围的增加最初会提高负载能力,达到最大值后再下降。同样,坡道高度的增加最初也会提高承载能力,达到最大值后随之减小。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Lubricants
Lubricants Engineering-Mechanical Engineering
CiteScore
3.60
自引率
25.70%
发文量
293
审稿时长
11 weeks
期刊介绍: This journal is dedicated to the field of Tribology and closely related disciplines. This includes the fundamentals of the following topics: -Lubrication, comprising hydrostatics, hydrodynamics, elastohydrodynamics, mixed and boundary regimes of lubrication -Friction, comprising viscous shear, Newtonian and non-Newtonian traction, boundary friction -Wear, including adhesion, abrasion, tribo-corrosion, scuffing and scoring -Cavitation and erosion -Sub-surface stressing, fatigue spalling, pitting, micro-pitting -Contact Mechanics: elasticity, elasto-plasticity, adhesion, viscoelasticity, poroelasticity, coatings and solid lubricants, layered bonded and unbonded solids -Surface Science: topography, tribo-film formation, lubricant–surface combination, surface texturing, micro-hydrodynamics, micro-elastohydrodynamics -Rheology: Newtonian, non-Newtonian fluids, dilatants, pseudo-plastics, thixotropy, shear thinning -Physical chemistry of lubricants, boundary active species, adsorption, bonding
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