IP Library Granted Patent US 10,486,389
Granted Patent B2
US 10,486,389 · App. 15/286,478 · Granted Nov 26, 2019

Laser-perforated metal honeycomb material and method of manufacturing same

Inventors: Christopher Davin (Playa Vista, CA); William B. Riley (Torrance, CA)
Assignee: Space Exploration Technologies Corp.
B32B3/12B32B3/266B32B15/00B32B37/146B32B38/0004B32B37/0076B32B37/1292B32B2311/00F01N3/2814F01N3/2821F01N2330/02F01N2330/04
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Quick Facts
Patent No.
US 10,486,389
App. No.
15/286,478
Granted
Nov 26, 2019
Kind
B2
Abstract

In one embodiment of the present disclosure, a method of manufacturing perforated metal honeycomb material includes: printing a roll of metal foil with adhesive; laser perforating the roll of metal foil to provide a plurality of holes in the metal foil; sheeting the printed and perforated roll of metal foil into a plurality of stacked sheets; and laminating the sheets of metal foil into a honeycomb before expansion block (HOBE). In another embodiment of the present disclosure, a perforated metal honeycomb structure includes a metal honeycomb structure having a plurality of laser-drilled holes wherein at least some of the plurality of holes are non-uniform in size, shape, and/or spacing between holes.

Claims (28)

1. A method of manufacturing perforated metal honeycomb material, the method comprising:

printing a roll of metal foil with lines of adhesive;

laser perforating the roll of metal foil to provide a plurality of holes in the metal foil;

after laser perforating, sheeting the printed and perforated roll of metal foil into a plurality of stacked sheets, wherein the lines of adhesive of each sheet are superposed with the lines of adhesive of a juxtaposed sheet; and

laminating the sheets of metal foil into a honeycomb before expansion block (HOBE).

2. The method of claim 1 , further comprising cutting the HOBE block into a plurality of HOBE slices.

3. The method of claim 2 , further comprising expanding the HOBE slices into expanded honeycomb structures having a plurality of perforations.

4. The method of claim 1 , wherein the roll of metal foil is printed with adhesive prior to laser perforation.

5. The method of claim 1 , wherein the roll of metal foil is printed with adhesive after laser perforation.

6. The method of claim 1 , wherein at least some of the plurality of holes are larger than 0.10 mm in diameter.

7. The method of claim 1 , wherein at least some of the plurality of holes are non-uniform in size and/or shape.

8. The method of claim 1 , wherein a spacing between at least some of the plurality of holes is non-uniform.

9. The method of claim 1 , further comprising corrugating the roll of metal foil to produce a corrugated honeycomb structure.

10. The method of claim 1 , wherein the method of manufacturing perforated metal honeycomb material does not include the process step of compression of the metal foil after the perforation process step.

11. A method of manufacturing perforated metal honeycomb material, the method comprising:

printing a roll of metal foil with lines of adhesive;

laser perforating the roll of metal foil to provide a plurality of holes in the metal foil;

after laser perforating, sheeting the printed and perforated roll of metal foil into a plurality of stacked sheets, wherein the lines of adhesive of each sheet are superposed with the lines of adhesive of a juxtaposed sheet;

laminating the sheets of metal foil into a honeycomb before expansion block (HOBE);

cutting the HOBE block into a plurality of HOBE slices; and

expanding the HOBE slices into expanded honeycomb structures having a plurality of perforations.

12. The method of claim 1 , where the holes produced by laser perforating have a volcano height of less than or about 30 μm.

13. The method of claim 1 , where the holes produced by laser perforating have a volcano height of less than or about 20 μm.

14. The method of claim 1 , where the holes produced by laser perforating have a volcano height of less than or about 1.8 μm.

15. The method of claim 1 , where the holes produced by laser perforating have a volcano height of about 1.8 μm to about 30 μm.

16. The method of claim 1 , where the laser perforating comprises using a nano IR laser.

17. The method of claim 1 , where the laser perforating comprises using a nano UV laser.

18. The method of claim 1 , where the laser perforating comprises using a femto Green laser.

Assignments (8)
RELEASE OF SECURITY INTEREST Recorded Feb 14, 2025
From: BANK OF AMERICA, N.A.
To: SPACE EXPLORATION TECHNOLOGIES CORP.
Reel/Frame 070237/0157 →
CERTIFICATE OF CONVERSION (STATE OF DELAWARE TO STATE OF TEXAS; NEW FILE NO.: 805421124 ; FILED: 02-14-2024) Recorded Feb 12, 2025
From: SPACE EXPLORATION TECHNOLOGIES CORP.
To: SPACE EXPLORATION TECHNOLOGIES CORP.
Reel/Frame 070203/0322 →
SECURITY AGREEMENT Recorded Feb 18, 2020
From: SPACE EXPLORATION TECHNOLOGIES CORP.
To: BANK OF AMERICA, N.A.
Reel/Frame 051952/0699 →
RELEASE OF SECURITY INTEREST Recorded Dec 18, 2019
From: BANK OF AMERICA, N.A. AS ADMINISTRATIVE AGENT
To: SPACE EXPLORATION TECHNOLOGIES CORP.
Reel/Frame 051322/0076 →
CORRECTIVE ASSIGNMENT TO CORRECT THE RECEIVING PARTY NAME PREVIOUSLY RECORDED AT REEL: 41114 FRAME: 504. ASSIGNOR(S) HEREBY CONFIRMS THE ASSIGNMENT. Recorded Oct 16, 2019
From: DAVIN, CHRISTOPHER; RILEY, WILLIAM B.
To: SPACE EXPLORATION TECHNOLOGIES CORP.
Reel/Frame 050734/0206 →
SECURITY AGREEMENT Recorded Nov 21, 2018
From: SPACE EXPLORATION TECHNOLOGIES CORP.
To: BANK OF AMERICA, N.A.
Reel/Frame 047618/0430 →
SECURITY AGREEMENT Recorded Feb 16, 2018
From: SPACE EXPLORATION TECHNOLOGIES CORP.
To: GOLDMAN SACHS BANK USA
Reel/Frame 045349/0426 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Dec 21, 2016
From: DAVIN, CHRISTOPHER; RILEY, WILLIAM B.
To: SPACE EXPLORATION TECHNOLOGIES CORPORATION
Reel/Frame 041114/0504 →
Continuity (1)
Related Publication 20180093443A1 · Apr 5, 2018