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Individual contributions of each gear error in the form of amplitude and frequency modulations are illustrated through an example analysis.
A new method to identify modal parameters (natural frequency and damping) and the equivalent gear error of a spur gear pair is introduced.
Because the gear errors which are introduced into LTCA model are measured along the line of action, the gear error values of helical gears must be converted to the normal direction as follows: f_{text{pbn}} = f_{text{pt}} cos alpha_{text{t}} cos beta_{text{b}}, (9 where fpbn is the pitch deviation in the direction of line of action.
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It is found that the influences of gear errors on system vibration are significant.
Gear errors on the plane of action are shown in Figure 4.
Open image in new window Figure 4 Schematic diagram of gear errors on plane of action.
The amplitude of gear errors is 26.71 μm when the accuracy of driving gear is sixth grade.
It can be observed that the LCMS is related to TVMS, distribution of gear errors and applied force.
Time-varying mesh stiffness (TVMS) and gear errors include short-term and long-term components are the two main internal dynamic excitations for gear transmission.
Matsumura et al. [9] developed a torsional dynamic model of helical gear system, and studied the gear errors on system vibration under lighter loading condition.
A equivalent meshing error analysis on different types of gear errors in the external and internal meshing line for star gearing system respectively.
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