首页> 外文会议>AHS 59th Annual Forum Proceedings Vol.2; May 6-8, 2003; Phoenix, Arizona >Spiral Bevel Pinion Crack Detection in a Helicopter Gearbox
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Spiral Bevel Pinion Crack Detection in a Helicopter Gearbox

机译:直升机齿轮箱中的螺旋锥齿轮裂纹检测

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The vibration resulting from a cracked spiral bevel pinion was recorded and analyzed using existing Health and Usage Monitoring System (HUMS) techniques. A tooth on the input pinion to a Bell OH-58 main rotor gearbox was notched and ran for an extended period at severe over-torque condition to facilitate a tooth fracture. Thirteen vibration-based diagnostic metrics were calculated throughout the run. After 101.41 hours of run time, some of the metrics indicated damage. At that point a visual inspection did not reveal any damage. The pinion was then run for another 12 minutes until a proximity probe indicated that a tooth had fractured. This paper discusses the damage detection effectiveness of the different metrics and a comparison of effects of the different accelerometer locations.
机译:使用现有的“健康和使用情况监视系统”(HUMS)技术记录并分析了破裂的螺旋锥齿轮引起的振动。将贝尔小齿轮OH-58主旋翼齿轮箱的输入小齿轮上的齿切开,并在严重的过转矩条件下长时间运行,以促进牙齿破裂。在整个运行过程中,计算了十三项基于振动的诊断指标。经过101.41小时的运行时间后,某些指标表明已损坏。那时,目视检查未发现任何损坏。然后将小齿轮再运行12分钟,直到接近探针表明牙齿已断裂。本文讨论了不同指标的损伤检测效果,并比较了不同加速度计位置的影响。

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