Metrology system for generating measurements of fuselage sections

Patent metadata

Field	Value
Publication number	US-9453720-B2
Application number	US-201414489057-A
Country	US
Kind code	B2
Filing date	Sep 17, 2014
Priority date	Sep 17, 2014
Publication date	Sep 27, 2016
Grant date	Sep 27, 2016

Abstract

A method and apparatus for processing fuselage sections. A scanning system is positioned between a first fuselage section held in a first cradle and a second fuselage section held in a second cradle. A group of beams of light is transmitted from the scanning system to targets on a first interior surface of the first fuselage section and a second interior surface of the second fuselage section. A reflected light is detected from a beam of light. Measurements of the first fuselage section and the second fuselage section are generated from using the reflected light generated in response to the beam of light. The measurements enable shaping at least one of the first fuselage section and the second fuselage section for joining the first fuselage section to the second fuselage section.

First claim

What is claimed is:

1. A method for measuring fuselage sections, the method comprising:
positioning a scanning system between a first fuselage section held in a first cradle and a second fuselage section held in a second cradle;
transmitting a group of beams of light from the scanning system to targets on a first interior surface of the first fuselage section and a second interior surface of the second fuselage section;
detecting, using the scanning system, a reflected light from the group of beams of light;
generating, using the scanning system, measurements of the first fuselage section and the second fuselage section from using the reflected light generated in response to the group of beams of light;
shaping, using the first cradle, the first fuselage section based on the measurements; and
joining, using the first cradle, the first fuselage section to the second fuselage section.

2. The method of claim 1 further comprising:
placing the targets on the first interior surface of the first fuselage section and the second interior surface of the second fuselage section.

3. The method of claim 1 , wherein generating the measurements comprises:
identifying a current shape of the first fuselage section and the second fuselage section.

4. The method of claim 3 , wherein generating the measurements comprises:
identifying a difference between the current shape of the first fuselage section and a desired shape for the first fuselage section.

5. The method of claim 3 , wherein the current shape is a first current shape and a desired shape is based on at least one of the first current shape of the first fuselage section and a second current shape of the second fuselage section or parameters specified by a design for the first fuselage section.

6. The method of claim 4 , wherein the current shape and the desired shape are contours for the first fuselage section.

7. The method of claim 1 further comprising:
repeating transmitting the group of beams of light from the scanning system to the targets on the first interior surface of the first fuselage section and the second interior surface of the second fuselage section; detecting the reflected light from the group of beams of light; and generating the measurements of the first fuselage section and the second fuselage section from using the reflected light generated in response to the group of beams of light, wherein the measurements enable shaping at least one of the first fuselage section and the second fuselage section for joining the first fuselage section to the second fuselage section each time a current shape of the first fuselage section is changed.

8. The method of claim 1 , wherein the scanning system is an optical metrology system and includes at least one of a lidar system or a laser scanning system.

9. The method of claim 1 further comprising:
sending the measurements from the scanning system to a controller that identifies forces needed to change a current shape of the first fuselage section to a desired shape for connecting the first fuselage section to the second fuselage section and sends commands to a cradle system to apply the forces to change the current shape of the first fuselage section towards the desired shape.

10. The method of claim 1 , wherein the measurements are generated without the scanning system contacting the first fuselage section and the second fuselage section.

11. The method of claim 1 , wherein the scanning system and the targets form a metrology system.

12. A method for measuring fuselage sections, the method comprising:
positioning a scanning system between a first fuselage section held in a first cradle and a second fuselage section held in a second cradle; and
generating, using the scanning system, measurements of the first fuselage section and the second fuselage section using the scanning system;
shaping, using the first cradle, the first fuselage section based on the measurements; and
joining, using the first cradle, the first fuselage section to the second fuselage section.

13. The method of claim 12 further comprising:
placing targets on a first interior surface of the first fuselage section and a second interior surface of the second fuselage section.

14. The method of claim 12 further comprising:
sending the measurements from the scanning system to a controller that identifies forces needed to change a current shape of the first fuselage section to a desired shape for connecting the first fuselage section to the second fuselage section and sends commands to a cradle system to apply the forces to change the current shape of the first fuselage section towards the desired shape.

15. The method of claim 12 , wherein the generating step comprises:
transmitting a beam of light from the scanning system to targets on a first interior surface of the first fuselage section and a second interior surface of the second fuselage section;
detecting reflected light from the beam of light; and
generating the measurements of the first fuselage section and the second fuselage section from using the reflected light generated in response to the beam of light.

16. The method of claim 12 , wherein the scanning system is an optical metrology system and includes at least one of a lidar system or a laser scanning system.

17. A metrology system for measuring fuselage sections, the metrology system comprising:
a scanner that transmits a group of beams of light from the scanning system to targets on a first interior surface of a first fuselage section and a second interior surface of a second fuselage section; detects a reflected light from the beam of light; and generates measurements of the first fuselage section and the second fuselage section from using the reflected light generated in response to the beam of light; and
a cradle system configured to shape the first fuselage system based on the measurements and join the first fuselage section to the second fuselage section.

18. The metrology system of claim 17 , wherein the scanner sends the measurements to a controller that identifies forces needed to change a current shape of the first fuselage section to a desired shape for connecting the first fuselage section to the 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.

19. The metrology system of claim 17 , wherein the group of beams of light is a group of laser beams.

20. The metrology system of claim 17 further comprising:
the targets, wherein the targets are selected from at least one of a reflective tape, a tooling ball, or a feature on one of the first fuselage section and the second fuselage section.

Assignees

• Boeing Co

Inventors

• Hunt Jeffrey H
• Walls Stephen A
• Whelan David Arthur
• Saint Clair Jonathan M

Classifications

• B64C1/069

  Joining arrangements therefor · CPC title

• B64F5/0009

  Operations & Transport · mapped topic

• G01B11/24 Primary

  for measuring contours or curvatures · CPC title

• B64F5/10

  Manufacturing or assembling aircraft, e.g. jigs therefor · CPC title