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Fundamental Investigation on the Tribological Failure Mechanisms of Compressor Surfaces, Scuffing: Detailed Roughness Analysis of Al390-T6

机译:压缩机表面摩擦磨损机理的基本研究,磨损:al390-T6的详细粗糙度分析

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摘要

Scuffing that occurs at tribological contacts in mechanical components, brings about topographical,chemical, and mechanical changes mainly at the sub-micron surface. In this project, extensive studies involving theuse of various engineering and scientific tools were performed to better understand the exact mechanisms behindthis phenomenon. A High Pressure Tribometer (HPT) was used to simulate shoe-on-disk tribological contacts undervarious conditions as encountered in compressor surfaces. Specifically, Al390-T6 disk/52100 steel pin tribo-pairsare representative of typical contacting surfaces used in swash plate-type air-conditioning compressors. Once thetime to scuff a sample under the test protocol was determined, subsequent HPT tests were stopped at 0.25 x ScuffingTime, 0.50 x Scuffing Time, and 0.75 x Scuffing Time intervals. The progressive change in disk topography leadingup to scuffing was first observed in the 1-D roughness study [1], but more extensively captured by the 2-DBirmingham-14 roughness characterization that is also described in this report [2]. When the chemical analyseswere conducted on the uppermost surfaces for depths of 120 nm, significant changes in some of the major chemicalelement concentration were revealed at scuffing. The major chemical compositional changes include a depletion ofsilicon, which was used to strengthen the aluminum alloy, and a drastic increase of oxygen component, signalingheavy oxidation at scuffing [1]. The mechanical properties of the disks undergoing tribological evolution were alsoinvestigated through various experimental hardness measurements, ranging from macro- to micro-, and to nanoscales[3]. Based on the experimental hardness results, it was found that the hardness of the material becomeshigher at the micro- and sub-micro scales than the bulk, regardless of the amount of wear towards scuffing. It wasalso observed that there was a gradual weakening of the uppermost 60 nm. In this report, we describe in detail thesurface roughness changes that occur to the Al390-T6 samples as they undergo progressively longer tribologicaltesting, eventually leading to scuffing.[1] Patel, J.J., Polycarpou, A.A., and Conry, T.F., 2002, ???Investigation of the Scuffing Mechanism Under StarvedLubrication Conditions Using Macro, Meso, Micro, and Nano Analytical Techniques,??? ACRC TR-191,University of Illinois.[2] Suh, A.Y., Polycarpou, A.A., Conry, T.F., 2003, ???Detailed Surface Roughness Characterization ofEngineering Surfaces Undergoing Tribological Testing Leading to Scuffing,??? Wear, in press.[3] Pergande, S.R., Polycarpou, A.A., and Conry, T.F., 2002, ???Use of Nano-Indentation and Nano-ScratchTechniques to Investigation Near Surface Material Properties Associated with Scuffing of EngineeringSurface,??? ACRC TR-193, University of Illinois.
机译:机械组件的摩擦接触处发生的划痕主要在亚微米表面引起形貌,化学和机械变化。在该项目中,进行了广泛的研究,涉及各种工程和科学工具的使用,以更好地了解这种现象背后的确切机制。高压摩擦计(HPT)用于模拟在压缩机表面遇到的各种条件下的磁盘摩擦靴接触。具体来说,Al390-T6圆盘/ 52100钢销摩擦对是斜盘式空调压缩机中典型的接触面的代表。一旦确定了在测试方案下磨损样品的时间,便会以0.25 x ScuffingTime,0.50 x Scuffing Time和0.75 x Scuffing Time间隔停止后续的HPT测试。在1-D粗糙度研究中[1]首次观察到导致磁盘划伤的磁盘形貌逐渐变化,但在本报告中也描述了2-DBirmingham-14粗糙度特征[2]。当在最上层表面进行深度为120 nm的化学分析时,划伤时发现某些主要化学元素浓度发生了显着变化。主要的化学成分变化包括用于增强铝合金强度的硅损耗,以及氧含量的急剧增加,表明划伤时发生了严重的氧化[1]。还通过各种实验硬度测量来研究经历了摩擦学演变的磁盘的机械性能,从宏观到微米,再到纳米级[3]。根据实验的硬度结果,发现在微观和亚微观尺度上,材料的硬度都比块体高,而与磨损的磨损量无关。还观察到最上面的60nm逐渐减弱。在此报告中,我们详细描述了Al390-T6样品在经历更长的摩擦学测试并最终导致划伤时发生的表面粗糙度变化。[1] Patel,J.J.,Polycarpou,A。和Conry,T.F.,2002,利用宏观,中观,微观和纳米分析技术研究饥饿润滑条件下的划痕机理。伊利诺伊大学ACRC TR-191。[2] Suh,A.Y.,Polycarpou,A.A.,Conry,T.F.,2003,``经过摩擦学测试导致划伤的工程表面的详细表面粗糙度表征,''报刊上穿着。[3] Pergande,S.R.,Polycarpou,A.A.和Conry,T.F.,2002,《使用纳米压痕和纳米划痕技术研究与EngineeringSurface划痕有关的近表面材料性能,??? ACRC TR-193,伊利诺伊大学。

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