Forming a complexly curved metallic sandwich panel

Patent metadata

Field	Value
Publication number	US-10239141-B2
Application number	US-201414511767-A
Country	US
Kind code	B2
Filing date	Oct 10, 2014
Priority date	Oct 10, 2013
Publication date	Mar 26, 2019
Grant date	Mar 26, 2019

Abstract

Aspects of the disclosure are directed to a bonding of a first skin and a second skin to a core material, coupling a sheet to the first skin to form with the first skin an enclosure containing the second skin and the core material, exposing the first skin, the second skin, and the core material to heat, and based on the exposition of heat, applying pressure via the enclosure to the first skin to cause the first skin to deform and expand to a shape of a die.

First claim

I claim:

1. A method comprising:
bonding a first skin and a second skin to a core material, wherein the core material comprises a honeycomb core;
coupling a sheet directly to the first skin to form with the first skin an enclosure between the sheet and the first skin, the second skin and the core material arranged within the enclosure and between the sheet and the first skin;
exposing the first skin, the second skin, and the core material to heat; and
based on the exposition of heat, applying pressure via the enclosure to the first skin to cause the first skin to deform and expand to a shape of a die.

2. The method of claim 1 , wherein the pressure is applied when the first skin, the second skin, and the core material reach a threshold temperature suitable for super plastic forming.

3. The method of claim 1 , wherein the pressure is applied through the insertion of an inert gas into the enclosure.

4. The method of claim 1 , wherein at least one of the core material includes holes between cells or the second skin is perforated.

5. The method of claim 1 , wherein the heat is applied using a vacuum furnace.

6. The method of claim 1 , further comprising:
removing excess material from a perimeter of the first skin; and
decoupling the sheet from the first skin.

7. The method of claim 1 , wherein the bonding comprises at least one of welding, brazing, or diffusion bonding.

8. The method of claim 1 , wherein the bonding occurs inside a forming tool configured to cause the first skin to deform and expand to the shape of the die, the method further comprising:
raising the pressure of air outside of the enclosure to bond the first and second skins and the core material.

9. The method of claim 1 , further comprising forming a barrel portion for an inner fixed structure of a thrust reverser, wherein the barrel portion comprises the first skin, the second skin and the core material.

10. The method of claim 9 , further comprising bonding bifurcation panels to the barrel portion.

11. The method of claim 1 , further comprising:
evacuating the enclosure of air.

12. The method of claim 11 , wherein the evacuation of the enclosure occurs prior to the exposition of heat.

13. The method of claim 1 , further comprising:
forming at least one of the first skin, the second skin, or the core material out of titanium.

14. The method of claim 1 , further comprising:
forming the first skin, the second skin, and the core material out of titanium.

15. A method, comprising:
bonding a first skin and a second skin to a core material, wherein the core material comprises a plurality of cavities that extend completely through the core material between the first skin and the second skin;
coupling a sheet to the first skin to form with the first skin an enclosure in which the second skin and the core material are positioned, wherein the second skin and the core material are between the first skin and the sheet, and the coupling between the sheet and the first skin is independent of the second skin and the core material;
heating the first skin, the second skin and the core material; and
applying pressure via the enclosure to the first skin to cause the first skin to deform and expand to a shape of a die, wherein the die contacts the first skin.

16. The method of claim 15 , further comprising decoupling the sheet from the first skin after the applying pressure via the enclosure to the first skin.

17. The method of claim 15 , wherein the core material includes holes between cells.

18. The method of claim 15 , wherein
the core material is vertically between the first skin and the second skin; and
the second skin comprises a plurality of perforations, and each of the plurality of perforations extends vertically through the second skin.

19. The method of claim 15 , wherein the sheet is coupled directly to the first skin.

Assignees

• Hamilton Sundstrand Corp
• Rohr Inc

Inventors

• Douglas Alan R

Classifications

• F05D2230/236

  Diffusion bonding · CPC title

• B21D47/00

  Making rigid structural elements or units, e.g. honeycomb structures · CPC title

• B23K31/02

  relating to soldering or welding · CPC title

• F05D2300/133

  Titanium · CPC title

• F05D2230/237

  Brazing · CPC title