Method to fixture and inspection contoured aerodynamic surfaces

Patent metadata

Field	Value
Publication number	US-9347759-B2
Application number	US-201313943972-A
Country	US
Kind code	B2
Filing date	Jul 17, 2013
Priority date	Jul 17, 2013
Publication date	May 24, 2016
Grant date	May 24, 2016

Abstract

A method to fixture and inspect contoured aerodynamic surfaces of a part, such as an engine inlet lip skin, is provided. A controlled preload is applied to one or more discrete locations along the contoured surface to constrain the lip skin at the locations the lip skin would be constrained upon assembly on the airplane. The contoured surfaces are then inspected to dimensional requirements. The controlled preload can be applied by use of magnets or elastic bumpers.

First claim

The invention claimed is:

1. A method comprising:
applying a controlled preload to one or more discrete locations along a contoured surface of a part to constrain the contoured surface to a shape formed in a final assembly, the discrete locations corresponding to points of attachment on the part when assembled with another component to form the final assembly; and
inspecting said contoured surface to dimensional requirements.

2. The method of claim 1 , wherein said controlled preload is applied using magnets.

3. The method of claim 1 , wherein said controlled preload is applied using elastic bumpers which engage with said part.

4. The method of claim 1 , further comprising:
mounting said part on a fixture to engage said part with said fixture, wherein the fixture generally conforms in shape to the contoured surface of the part.

5. The method of claim 4 , wherein the fixture includes magnets on said fixture at the discrete locations, and wherein the method further comprises:
after said part is mounted on said fixture, applying magnets to an external face of said part, said magnets interacting with said magnets on said fixture to further engage said part with said fixture to apply said controlled preload.

6. The method of claim 4 , wherein the fixture includes elastic bumpers on said fixture at the discrete locations, and
wherein said part engages with said elastic bumpers when said part is mounted on said fixture to apply said controlled preload.

7. The method of claim 4 , further comprising:
wherein after mounting said part on said fixture, applying a force onto said part to cause said part to move into further engagement with said fixture.

8. The method of claim 7 , wherein said force is applied by placing sandbags on said part.

9. The method of claim 7 , wherein said force is applied by attaching bungee cords to a fixed structure and over said part.

10. The method of claim 7 , wherein said force is applied by magnets positioned at a different location on said fixture than said discrete locations.

11. The method of claim 7 , wherein said force is removed prior to inspecting said contoured surface to dimensional requirements.

12. The method of claim 1 , wherein said inspecting IS performed using photogrammetry.

13. A method of inspecting a part having a contoured surface, the method comprising:
engaging the part with a fixture having a shape which generally conforms to the contoured surface of the part;
applying a controlled preload to one or more discrete locations along the contoured surface to constrain the contoured surface to a shape formed in a final assembly on the fixture, the discrete locations corresponding to points of attachment on the part when assembled with another component to form the final assembly; and
inspecting the contoured surface to dimensional requirements.

14. The method of claim 13 , further including
positioning magnets on the fixture and corresponding magnets on the part in the discrete locations to apply the controlled preload.

15. The method of claim 13 , wherein the controlled preload is applied toward the fixture using magnets.

16. The method of claim 13 , wherein the part is an aircraft part.

17. A method of inspecting an aircraft part comprising:
applying a controlled preload to one or more discrete locations along a flexible contoured surface of the aircraft part to constrain the contoured surface to a fixture in a shape the aircraft part assumes when assembled on the aircraft, the discrete locations corresponding to points of attachment on the aircraft part when assembled on the aircraft; and
inspecting the contoured surface to dimensional requirements.

18. The method of claim 17 , further including positioning magnets on the fixture and corresponding magnets in the discrete locations to apply the controlled preload.

Assignees

• Boeing Co

Inventors

• Kane Daniel J

Classifications

• B64F5/0045

  Operations & Transport · mapped topic

• B64F5/00 Primary

  Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for · CPC title

• G01B5/00 Primary

  Measuring arrangements characterised by the use of mechanical techniques · CPC title

• G01M5/005

  by means of external apparatus, e.g. test benches or portable test systems · CPC title

• G01M5/0091

  by using electromagnetic excitation or detection · CPC title