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Tooth Flank Fracture - Influence of Macro and Micro Geometry

机译:牙齿侧面骨折 - 宏观和微观几何的影响

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A not so often seen failure mode for gears is tooth flank fracture. It is observed on cylindrical and bevel gears, especially but not exclusively on case carburized gears. The characteristic of the damage is a crack initiation in the region of the active contact area and inside the material, with a crack propagation to the surface of the loaded flank and in the direction of the root area on the other side of the tooth. Most of the cases mentioned in literature occurred on gears with a larger module. The main influence parameters are the local Hertzian contact stress and the hardness profile. The pressure on the flank causes crack initiation below the surface, typically at a preexisting material fault. The crack grows in two directions, into the core of the tooth and towards the surface of the flank. Secondary cracks might occur that are oriented in an angle to the original crack. Typically as soon as the crack is visible the tooth breaks. This is a difference to the root fracture, where the crack initiates at the surface and special ink can be used to find cracks before the gear totally fails. For tooth flank fracture a new standard is in progress, ISO DTS 19042 [3]. It is in the very early stages, however, the outline of the method itself is already quite fixed. It is based on the work from Witzig [6], which itself goes back to Annast [4] and Bruckmeier [5]. This paper refers to the version from 18th of February, 2015. Since changes are currently very frequent, some of the observations below might already be outdated. The method as far as it is developed now is based on a local analysis of the Hertzian contact stress and the hardness profile at arbitrary points of the active area of the tooth flank. Therefore the integration of the calculation in the gear contact analysis is a natural way of implementing it. Along with the functions to vary parameters this is a suitable platform to gain first experiences with the new method and to perform sensitivity studies. The paper presents the first results obtained from a systematic variation of gear parameters, to show the influence of these parameters as modeled by the method.
机译:A不经常看到齿轮的故障模式是牙齿侧面裂缝。在圆柱形和锥齿轮上观察到,特别是但在碳钢齿轮上仅限于外壳。损伤的特性是在主动接触面积和材料内部的区域中的裂缝开始,其裂缝传播到装载的侧面的表面和齿的另一侧的根区域的方向。文献中提到的大多数病例发生在具有更大模块的齿轮上。主要影响参数是局部赫兹接触应力和硬度曲线。侧翼上的压力导致表面以下的裂纹引发,通常在预先存在的材料故障下。裂缝在两个方向上生长,进入牙齿的核心并朝向侧面的表面。可能发生次要裂缝,其成导到原始裂缝的角度。通常一旦裂缝可见牙齿断裂。这与根部骨折的差异,其中在表面和特殊墨水处的裂缝引发可用于在齿轮完全失败之前找到裂缝。对于牙齿侧翼骨折,新标准正在进行中,ISO DTS 19042 [3]。然而,它处于早期阶段,但是,该方法本身的轮廓已经完全固定。它基于Witzig [6]的工作,它本身返回Annast [4]和Bruckmeier [5]。本文是指2015年2月18日的版本。由于目前的变化非常频繁,以下一些观察可能已经过时了。如现在开发的方法基于牙齿侧翼的有源区域的任意点的局部分析。牙齿的局部接触应力和硬度曲线。因此,在齿轮接触分析中的计算集成是实现它的自然方式。随着改变参数的功能,这是一个合适的平台,用于获得新方法和执行灵敏度研究的首次经验。本文提出了从齿轮参数的系统变化获得的第一个结果,以显示通过该方法的模型的这些参数的影响。

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