Patent ID: 8869367
Filing Date: 2014-10-28
Classification: B64F,Y10T

Abstract:
1. An aircraft structure manufacturing apparatus comprising: a first supporting unit configured to support a first portion of a positioning object; a second supporting unit configured to support a second portion of said positioning object; a third supporting unit configured to support a third portion of said positioning object; a fourth supporting unit configured to support a fourth portion of said positioning object; a servo system group; and a control unit configured to control said servo system group, wherein said servo system group comprises: wherein said positioning object is a jig configured to support a part of an aircraft structure, wherein said servo system group further comprises: wherein a first rotation axis parallel to said vertical direction and a first 2-axis gimbal are provided between said first supporting unit and said first portion, wherein a second rotation axis parallel to said vertical direction and a second 2-axis gimbal are provided between said second supporting unit and said second portion, wherein a third rotation axis parallel to said vertical direction, a third 2-axis gimbal and a 1-axis sliding mechanism are provided between said third supporting unit and said third portion, and wherein a fourth rotation axis parallel to said vertical direction, a fourth 2-axis gimbal and a 2-axis sliding mechanism are provided between said fourth supporting unit and said fourth portion.