Patent · US Active

Fuselage manufacturing system

US11131982B2 · kind B2 · utility

1Cited by
13References
20Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 17, 2014
Grant dateSep 28, 2021
Priority date
Expiry dateFeb 26, 2036

Classification

  • Technology area (CPC G)Physics
  • CPC primaryG05B2219/45071
  • WIPO fieldControl
  • WIPO sectorInstruments

Abstract

A method and apparatus for processing fuselage sections. The apparatus comprises a cradle system, a metrology system, and a controller. The cradle system holds a first fuselage section and applies forces to the first fuselage section to change a current shape of the first fuselage section. The metrology system makes measurements of the current shape of the first fuselage section. The controller receives the measurements from the metrology system, identifies the forces needed to change the current shape of the first fuselage section towards a desired shape for connecting the first fuselage section to a second fuselage section, and sends commands to the cradle system to apply the forces to change the current shape of the first fuselage section towards the desired shape.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.