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Geometrically Synchronized Measurements Method If a gear tooth is damaged, the assumption is that, when engaged, it produces a waveform that is distinctive from the average. However, the transmission’s vibrations spec-trum is complicated by the many simultaneously meshing gears, and often these details are obscured, even after time-synchronous averaging. As was shown in the previous sec-tions, special processing tools are needed to isolate the dy-namics in order to be able to apply condition indicators to the individual components. The technique relates subsets of the TSA signal to the individual sun teeth in mesh. Figure 23 shows an enlarged view of the sun gear region for the OH-58C con.guration. At any given time, the sun gear is in mesh with four plan-ets. Due to the non-sequential nature of the OH-58C, the engaged planets are in different meshing positions along each tooth making it dif.cult to determine which teeth are ”most in mesh.” To eliminate ambiguity, the lines of centers between the sun and planets are used as references. The centers of each planet are tracked during meshing and then mapped to a region on the sun tooth. The sun gear angles in mesh at any given time gives the center of each individual mesh bin whose width is one sun gear’s pitch. A group of simultaneously meshing mesh bins is called a mesh group. 直升机网 www.helicopter.cn 直升机翻译 www.aviation.cn 本文链接地址:Sun Gear Fault Detection on an OH-58C Helicopter Transmission(22) |