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Wear of tire tread/carcass composites

机译:轮胎胎面/胴体复合材料

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A multi-axial dynamic test instrument was designed to perform wear testing of actual aircraft tires as well as tread/carcass composite specimens under laboratory loading conditions which simulate the elements of take-off, landing and taxiing operations. The wear tester consists of a self-spinning abrading head, mounted on the actuator of a servo-hydraulic test system, which faces either (1) the tread surface of a composite specimen clamped by a horizontal stretch frame or (2) the tread region of actual inflated tires. The test concept has been partially proven in the case of tread/carcass composite specimens by building a prototype test apparatus and operating it successfully. In the current test set-up, the specimen is subjected to static tension to simulate a circumferential load in the tire footprint and the tread surface is in periodic contact with an abrading head under a specific level of pressure. A swirling mode of motion is superimposed to a spinning action of a circular disk type head to induce the wear of the tread side of the specimen in a constantly changing direction. This ensures the elimination of "abrasion pattern" and allows "intrinsic abrasive wear" under varied contact pressure. Repeatable trends of thickness reduction and weight loss characteristics were observed for each case of tread/carcass composites tested thus far in this study. In the case of automotive tire materials, our preliminary wear test results were found to be consistent with the field experience. The wear rate appeared to be governed by the particle size and the degree of agglomeration of carbon black fillers. The wear phenomenon may, therefore, be interpreted as a process of filler-matrix debonding under contact fatigue loading. One interesting observation was that, well below a critical temperature, higher temperatures tended to be associated with lower wear rates. The results clearly suggest that less hysteresis of tread compound causes more rapid tread wear, which is consistent with the model proposed by Schallamach and Turner.
机译:设计了多轴动态测试仪器,用于在实验室负载条件下执行实际飞机轮胎以及胎面/胴体复合标本的磨损测试,该条件模拟起飞,着陆和滑行运算的元素。磨损测试仪由自动旋转研磨头组成,安装在伺服液压试验系统的致动器上,该伺服液压试验系统的致动器面向由水平拉伸框架或(2)胎面区域夹紧的复合样品的胎面表面实际充气轮胎。通过构建原型测试装置并成功操作,在胎面/胴体复合标本的情况下部分证明了测试概念。在当前的测试设置中,样品经受静态张力,以模拟轮胎占地面积中的圆周载荷,并且在特定压力水平下,胎面表面与研磨头周期性接触。旋转运动模式叠加到圆盘式头部的旋转动作,以促使样品的胎面侧的磨损在不断变化的方向上。这确保了消除“磨损图案”并允许“固有磨损磨损”在不同的接触压力下。对于迄今为止测试的胎面/胎体复合材料的每种情况,观察到厚度减小和减肥特性的可重复趋势。在汽车轮胎材料的情况下,我们的初步磨损测试结果被发现与现场经验一致。磨损率似乎受到粒径和炭黑填料附聚度的管辖。因此,磨损现象可以被解释为在接触疲劳负荷下填充基质脱粘剂的过程。一个有趣的观察是,远低于临界温度,较高的温度往往与较低的磨损率相关。结果清楚地表明,胎面化合物的滞后导致更快的胎面磨损,这与Schallamach和特纳提出的模型一致。

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