Posture Alignment and Finishing System for Aircraft Wing

Hong Shuang Zhang

doi:10.4028/www.scientific.net/AMM.644-650.4956

Paper Titles

Preparation of High-Solids UV-Curable Actylate Pressure-Sensitive Adhesive with Low Viscosity for Printed Electronics
p.4936

Satellite Oilfield in High Water-Cut Stage New Composite Displacement System Research
p.4941

Intrinsic Safety Explosion-Proof System
p.4945

The Crystal Structure and Magnetic Property of Bi-Substituted Nd₂Fe_17-x-yTi_xSi_y Intermetallic Compounds
p.4950

Posture Alignment and Finishing System for Aircraft Wing
p.4956

Magneto-Thermal Simulation Analysis of the Sheet Metal in the Transverse Flux Induction Heating Process
p.4960

Applications of 3D Printing Technology in the Mechanical Manufacturing
p.4964

Analysis and Compensation Strategy of Non-Linear Error in Five-Axis CNC Machining
p.4967

Study on Deformation of Thin-Walled Workpieces Milling Machining Based on Finite Element Method
p.4971

HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 644-650Posture Alignment and Finishing System for...

Posture Alignment and Finishing System for Aircraft Wing

Abstract:

A novel posture alignment system based on 3-DOF locators is presented to meet the finishing need of big part such as wing after assembly. The system includes three locators for posture alignment and auxiliary clamping devices for auxiliary clamping. The structure and basic principle of device and the posture alignment principle are introduced in details. The application show the system could meet the posture alignment and finishing need of big part such as wing and provide a reference for aircraft assembly and fabrication.