Abstract

To accurately study the dynamic characteristics of the spiral bevel gear transmission system in a helicopter tail transmission system, the finite element model of the gear shaft was established by a Timoshenko beam element, and the mechanical model of the spiral bevel gear was created by the lumped mass method. The substructure method is employed to extract the dynamic parameters from the gearbox’s finite element model, and the dynamic model of the spiral bevel gear-shaft-bearing-gearbox coupling system was built according to the interface coordination conditions. In the model, the influences of time-varying stiffness, a time-varying transmission error, gearbox flexibility, unbalance excitation, and a flexible shaft and bearing support on the system vibration were taken into account simultaneously. On this basis, the dynamic differential equations of the full coupling system of the spiral bevel gear were derived, and the effects of the gearbox flexibility, the shaft angle, and the unbalance on the dynamic properties of the system were analysed. The results show that the gearbox flexibility can reduce the gear meshing force and bearing force, in which there is a more significant impact on the bearing force. The shaft angle affects the position, size, and direction of the system’s axis trajectory. Meanwhile, the meshing force and the bearing force of the system are also varied because of the various pitch angles of the driving and driven gears under different shaft angles. The unbalance of the gear shaft has an effect on the vibration of the spiral bevel gear transmission system in all directions, wherein the influence on the torsional vibration is the most significant, and the influence increases as the unbalance rises. The unbalance of the gear shaft also affects the meshing force and bearing force, which increases as the rotational speed rises. This research provides a theoretical basis to optimize dynamic performance and reduce the vibration and noise of a spiral bevel gear full coupling system.

Highlights

  • To accurately study the dynamic characteristics of the spiral bevel gear transmission system in a helicopter tail transmission system, the finite element model of the gear shaft was established by a Timoshenko beam element, and the mechanical model of the spiral bevel gear was created by the lumped mass method. e substructure method is employed to extract the dynamic parameters from the gearbox’s finite element model, and the dynamic model of the spiral bevel gear-shaft-bearing-gearbox coupling system was built according to the interface coordination conditions

  • The meshing force and the bearing force of the system are varied because of the various pitch angles of the driving and driven gears under different shaft angles. e unbalance of the gear shaft has an effect on the vibration of the spiral bevel gear transmission system in all directions, wherein the influence on the torsional vibration is the most significant, and the influence increases as the unbalance rises. e unbalance of the gear shaft affects the meshing force and bearing force, which increases as the rotational speed rises. is research provides a theoretical basis to optimize dynamic performance and reduce the vibration and noise of a spiral bevel gear full coupling system

  • Analysis of the transient dynamics is carried out using finite element software to obtain the timevarying meshing stiffness of the spiral bevel gear pair because the tooth surface of the spiral bevel gear is a complex curved surface. en, the dynamic equation of the nonorthogonal spiral bevel gear transmission system is constructed via the finite element method and the lumped mass hybrid modelling method. e dynamic parameters of the gearbox system are extracted by the substructure method and are connected by the nodes of the bearing support, establishing the dynamic model of the spiral bevel gear-shaft-bearing-box coupling system

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Summary

Dynamic Equation of the Spiral Bevel Gear Full Coupling System

Calculation of the Meshing Stiffness of the Spiral Bevel Gear. It is difficult to calculate the meshing stiffness of the gear teeth using the theoretical analysis method because the tooth surface of the spiral bevel gear is a space meshing gear. E comprehensive elastic deformation δn and contact force Fn are calculated when multiple pairs of gears mesh at the same time, and the comprehensive meshing stiffness can be obtained directly. In order to improve the efficiency of calculation, nine pairs of gear teeth are selected from the spiral bevel gear pair for the meshing analysis. Each period T is divided into ten segments on average, and two meshing periods are taken. en, each Ki value at its

20 Box element
Conclusion
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