Method for producing a structural material stack

Patent metadata

Field	Value
Publication number	US-12448698-B2
Application number	US-202318183541-A
Country	US
Kind code	B2
Filing date	Mar 14, 2023
Priority date	Jul 15, 2022
Publication date	Oct 21, 2025
Grant date	Oct 21, 2025

Abstract

A method for producing a structural material stack includes forming a composite panel that includes a carbon fiber reinforced polymer (CFRP) material, and applying an interface film on an exterior composite surface of the composite panel. The interface film is electrically conductive. The method includes performing an electroplating process to form a metallic coating on the interface film such that the interface film is sandwiched between the composite panel and the metallic coating. The metallic coating has a different material composition than the interface film.

First claim

What is claimed is:

1. A method for producing a lipskin of an inlet cowl of an aircraft nacelle, the method comprising:
forming a composite panel that includes a carbon fiber reinforced polymer (CFRP) material, wherein the composite panel includes an exterior composite surface;
applying an interface film on the exterior composite surface of the composite panel, wherein the interface film is electrically conductive and has an interior interface surface and an exterior interface surface; and
performing an electroplating process to form a metallic coating on the exterior interface surface of the interface film such that the interface film is sandwiched between the composite panel and the metallic coating, the metallic coating having a different material composition than the interface film, thereby forming said lipskin, wherein the metallic coating defines an exterior surface of the inlet cowl along a leading edge of the inlet cowl.

2. The method of claim 1 , wherein the composite panel is formed to have a curved contour that represents at least a portion of an annular barrel shape.

3. The method of claim 1 , wherein the interface film is applied to the exterior composite surface of the composite panel via adhesive bonding.

4. The method of claim 1 , wherein the interface film is a ply that includes over 50% by weight of a metallic particulate.

5. The method of claim 4 , wherein the metallic particulate comprises silver.

6. The method of claim 1 , further comprising curing the composite panel and the interface film after applying the interface film and before performing the electroplating process.

7. A method for producing a structural material stack, the method comprising:
forming a composite panel that includes a carbon fiber reinforced polymer (CFRP) material, wherein the composite panel includes an exterior composite surface;
applying an interface film on the exterior composite surface of the composite panel, wherein the interface film is electrically conductive and has an interior interface surface and an exterior interface surface;
performing a nickel strike chemical process on the interface film after applying the interface film; and
performing an electroplating process to form a metallic coating on the exterior interface surface of the interface film after performing the nickel strike chemical process so the interface film is sandwiched between the composite panel and the metallic coating, the metallic coating having a different material composition than the interface film, thereby forming said structural material stack.

8. The method of claim 1 , wherein the electroplating process is performed such that the metallic coating that is formed comprises a nickel alloy composition.

9. The method of claim 8 , wherein the nickel alloy composition is a nickel cobalt (NiCo) alloy.

10. The method of claim 1 , further comprising laser drilling a plurality of perforations through the section of the lipskin, wherein the laser drilling comprises emitting a laser beam that penetrates the CFRP material of the composite panel before penetrating the interface film and the metallic coating.

11. A lipskin of an inlet cowl of an aircraft nacelle, the lipskin comprising:
a composite panel that includes a carbon fiber reinforced polymer (CFRP) material, wherein the composite panel includes an exterior composite surface;
an interface film bonded via an adhesive to the exterior composite surface of the composite panel, wherein the interface film is electrically conductive and has an interior interface surface and an exterior interface surface; and
a metallic coating formed on the exterior interface surface of the interface film such that the interface film is sandwiched between the composite panel and the metallic coating, the metallic coating having a different material composition than the interface film, wherein the metallic coating defines an exterior surface of the inlet cowl along a leading edge of the inlet cowl.

12. The lipskin of claim 11 , wherein the composite panel has a curved contour that represents at least a portion of an annular barrel shape.

13. The lipskin of claim 11 , wherein the interface film is a ply that includes over 50% by weight of a metallic particulate.

14. The lipskin of claim 13 , wherein the metallic particulate comprises silver.

15. The lipskin of claim 11 , wherein the metallic coating comprises a nickel alloy composition.

16. The lipskin of claim 15 , wherein the nickel alloy composition is a nickel cobalt (NiCo) alloy.

17. The lipskin of claim 11 , wherein the lipskin includes a plurality of perforations that each continuously extend through the composite panel, the interface film, and the metallic coating.

18. A method for producing an inlet cowl, the method comprising:
forming a composite panel that includes a carbon fiber reinforced polymer (CFRP) material, the composite panel including an exterior composite surface and formed to have a curved contour that represents at least a portion of an annular barrel shape;
applying an interface film on the exterior composite surface of the composite panel, wherein the interface film includes over 50% by weight of a metallic particulate; and
performing an electroplating process to form a metallic coating on the interface film such that the interface film is sandwiched between the composite panel and the metallic coating, the metallic coating having a nickel alloy composition which is different from a material composition of the interface film, wherein the metallic coating defines an exterior surface of the inlet cowl along a leading edge of the inlet cowl.

19. The method of claim 18 , further comprising performing a nickel strike chemical process on the interface film after applying the interface film and before performing the electroplating process.

20. The method of claim 18 , wherein the interface film includes over 50% by weight of silver.

Assignees

• Boeing Co
• Radius Aerospace Inc

Inventors

• Rust Charles William
• Weidler Iii John Alfred
• Qarni Muhammad Jawad
• Mannion Niall

Classifications

• C25D7/04

  Tubes; Rings; Hollow bodies · CPC title

• C25D3/562

  containing more than 50% by weight of iron or nickel or cobalt · CPC title

• B64D29/08

  Inspection panels for power plants · CPC title

• B23K26/402

  involving non-metallic material, e.g. isolators · CPC title

• B23K26/386

  of blind holes · CPC title