Abstract

Vibrations in the aircraft assembly building will affect the precision of the robotic drilling system. A variable stiffness and damping semiactive vibration control mechanism with quasi-zero stiffness characteristics is developed. The quasi-zero stiffness of the mechanism is realized by the parallel connection of four vertically arranged bearing springs and two symmetrical horizontally arranged negative stiffness elements. Firstly, the quasi-zero stiffness parameters of the mechanism at the static equilibrium position are obtained through analysis. Secondly, the harmonic balance method is used to deal with the differential equations of motion. The effects of every parameter on the displacement transmissibility are analyzed, and the variable parameter control strategies are proposed. Finally, the system responses of the passive and semiactive vibration isolation mechanisms to the segmental variable frequency excitations are compared through virtual prototype experiments. The results show that the frequency range of vibration isolation is widened, and the stability of the vibration control system is effectively improved without resonance through the semiactive vibration control method. It is of innovative significance for ambient vibration control in robotic drilling systems.

Highlights

  • In the aviation manufacturing field, a lot of drilling and riveting is required to be carried out for assembly [1]

  • In 1989, Alabuzhev systematically put forward a theory of a quasi-zero stiffness vibration control method and designed various mechanisms [17]

  • This paper develops a quasi-zero stiffness vibration control method for a robotic drilling system

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Summary

Introduction

In the aviation manufacturing field, a lot of drilling and riveting is required to be carried out for assembly [1]. As a typical nonlinear structure, the quasi-zero stiffness structure has characteristics of high static stiffness and low dynamic stiffness via the parallel connection of a positive and negative stiffness element It can effectively widen the vibration isolation frequency band and improve the vibration isolation efficiency of the system. In 1989, Alabuzhev systematically put forward a theory of a quasi-zero stiffness vibration control method and designed various mechanisms [17]. A vertical 2-DOF dynamic vibration absorber based on a quasi-zero stiffness mechanism was developed as well to abate the low-frequency vibration of high-speed trains in order to improve seat comfort [24]. This paper develops a quasi-zero stiffness vibration control method for a robotic drilling system.

Design
Passive Structural Parameters Analysis
Dynamic stiffness curves for
Dynamics Analysis and Modeling
Schematic
Stability Analysis
Effects of Damping Coefficient on Vibration Control Performance
Parameter Adjustment
Variable Stiffness Control
Variable Damping Control
13. Effect
Simulationparameter d
Simulation of the Vibration Control System with Variable Stiffness
Conclusions
Full Text
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