IP Library Granted Patent US 9,393,761
Granted Patent B2
US 9,393,761 · App. 13/832,181 · Granted Jul 19, 2016

Hybrid structure and methods for forming the same

Inventor: Marcus Alexander Erickson (Snohomish, WA)
Assignee: The Boeing Company
B32B17/1055B29C65/48B29C65/562B29C65/72B29C66/02242B29C66/1122B29C66/472B29C66/7212B29C66/7314B29C66/742B32B37/16C23F13/10B29C65/483B29C66/32B29C66/7422B29L2031/3002B29L2031/3076F16B33/008Y10T156/10
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Quick Facts
Patent No.
US 9,393,761
App. No.
13/832,181
Granted
Jul 19, 2016
Kind
B2
Abstract

A method for forming a hybrid structure is provided. The method includes applying a sealant to a first component fabricated from a first material, coupling an isolation sheet to the sealant, and coupling a second component to the isolation sheet. The isolation sheet and the second component are fabricated from a second material that is different than the first material to facilitate preventing formation of a galvanic cell within the hybrid structure.

Claims (34)

1. A method for forming a hybrid structure, said method comprising:

applying a sealant to a first component fabricated from a first material;

coupling an isolation sheet to the sealant, wherein the sealant has a thickness and covers a surface area of the first component such that the isolation sheet is separated from the first component;

forming at least one bore hole through at least one of the isolation sheet, the sealant, and the first component; and

coupling a second component to the isolation sheet with a fastener at the at least one bore hole, wherein the second component and the isolation sheet are both fabricated from a second material that is different than the first material to facilitate preventing formation of a galvanic cell within the hybrid structure.

2. The method in accordance with claim 1 further comprising:

selecting the first material to have a first electrode potential; and

selecting the second material to have a second electrode potential that is different than the first electrode potential.

3. The method in accordance with claim 1 further comprising:

coupling an isolating layer to a surface of the first component; and

applying the sealant to the isolating layer.

4. The method in accordance with claim 1 , wherein coupling an isolation sheet to the sealant comprises bonding the isolation sheet to the sealant with the sealant.

5. The method in accordance with claim 1 , wherein applying a sealant comprises applying a sealant that substantially prevents ingress of an electrolyte between the isolation sheet and the first component.

6. The method in accordance with claim 1 , wherein coupling an isolation sheet to the sealant comprises applying pressure to the isolation sheet to facilitate removing excess sealant from between the isolation sheet and the first component.

7. The method in accordance with claim 1 , wherein forming at least one bore hole further comprises:

aligning the second component with the isolation sheet in a predetermined orientation;

determining bore hole locations on the isolation sheet with at least one of holes defined in the second component and a drill jig; and

forming a plurality of bore holes through the isolation sheet, the sealant, and the first component at the hole locations.

8. The method in accordance with claim 7 , further comprising substantially maintaining alignment of the second component relative to the isolation sheet while the bore holes are formed.

9. The method in accordance with claim 1 , wherein coupling the second component to the isolation sheet comprises aligning the second component with the isolation sheet such that the second component remains separated from the first component.

10. A method for use in forming an assembly, said method comprising:

forming a sub-assembly that includes a first component fabricated from a first material, a sealant applied to the first component, and an isolation sheet coupled to the sealant, wherein the sealant is applied in a thickness and covers a surface area of the first component such that the isolation sheet is separated from the first component, and wherein the isolation sheet is fabricated from a second material that is different than the first material, to facilitate preventing formation of a galvanic cell within the assembly;

installing the sub-assembly in the assembly;

forming at least one bore hole through at least one of the isolation sheet, the sealant, and the first component; and

coupling a second component to the sub-assembly along the isolation sheet with a fastener at the at least one bore hole, wherein the second component is fabricated from the second material.

11. The method in accordance with claim 10 , wherein forming at least one bore hole comprises:

aligning the second component with the isolation sheet in a predetermined orientation; and

determining bore hole locations on the isolation sheet with at least one of holes defined in the second component and a drill jig.

12. The method in accordance with claim 11 further comprising:

forming bore holes through the sub-assembly at the hole locations.

13. The method in accordance with claim 12 , wherein using at least one fastener comprises applying a second sealant to at least one of the bore holes and the at least one fastener before using the at least one fastener.

14. The method in accordance with claim 10 further comprising:

selecting the first material to have a first electrode potential; and

selecting the second material to have a second electrode potential that is different than the first electrode potential.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 15, 2013
From: ERICKSON, MARCUS ALEXANDER
To: THE BOEING COMPANY
Reel/Frame 030009/0096 →
Continuity (1)
Related Publication 20140272429A1 · Sep 18, 2014