IP Library › Granted Patent US 11,608,174
Granted Patent B2
US 11,608,174 · App. 16/995,195 · Granted Mar 21, 2023

Power distribution panel

Inventors: Michael James Smith (Chadlington, GB); Alexander James Rainbow (Swindon, GB)
Assignee: GE Aviation Systems Limited
B64D1/00H05K5/0234H05K7/08H05K7/1452B64D2221/00
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Quick Facts
Patent No.
US 11,608,174
App. No.
16/995,195
Granted
Mar 21, 2023
Kind
B2
Abstract

A power distribution panel with a backplane, an insulating panel covering the backplane, and at least one electronic component mounted to the insulating panel. A set of feet can be mounted to the insulating panel and configured to absorb stress applied to the insulating panel where the set of feet are located in the same plane as the backplane.

Claims (23)

1. A power distribution panel comprising: a backplane comprising at least a portion having a cellular structure defining a plurality of voids;

at least one insulating panel covering at least some of the plurality of voids;

at least one electrical component mounted to the insulating panel;

a set of feet coupled to the insulating panel; wherein the set of feet are decoupled from the backplane; wherein the set of feet are mounted to a structure of a vehicle; wherein the set of feet are configured to absorb shear stress applied to the insulating panel; and

wherein at least a portion of the set of feet is located in the same plane as the backplane.

2. The power distribution panel of claim 1 , wherein the cellular structure is a honeycomb structure.

3. The power distribution panel of claim 1 , wherein the insulating panel is made with melamine.

4. The power distribution panel of claim 1 , wherein the cellular structure is made with aluminum.

5. The power distribution panel of claim 1 , wherein the plurality of voids are distributed throughout the backplane in an arrangement of shapes closely fitted together in a repeated pattern without gaps or overlapping.

6. A power distribution panel comprising: a backplane comprising at least a portion having a cellular structure defining a plurality of voids, at least one insulating panel covering at least some of the plurality of voids; at least one electronic component mounted to the insulating panel;

a set of feet mounted directly to the insulating panel and configured to absorb shear stress applied to the insulating panel; wherein the set of feet are located in the same plane as the backplane; wherein the set of feet is separate from the backplane;

wherein the set of feet are mounted to a structure of a vehicle; and

wherein the backplane is configured to absorb perpendicular stress applied to the backplane.

7. The power distribution panel of claim 6 , wherein the plurality of voids is distributed throughout the backplane in an arrangement of shapes closely fitted together in a repeated pattern without gaps or overlapping.

8. The power distribution panel of claim 6 , wherein the insulating panel is made with melamine.

9. The power distribution panel of claim 6 , wherein the cellular structure is made with aluminum.

10. A method of manufacturing a power distribution panel comprising: forming a cellular structure with a plurality of voids to define a backplane; covering the cellular structure with at least one insulating panel; mounting at least one electrical component to the insulating panels mounting a set of feet directly to the insulating panel to absorb shear stress applied to the insulating panel; and

wherein the set of feet is located in the same plane as but separate from the backplane, and further comprising mounting the set of feet to a vehicle.

11. The method of claim 10 , further comprising mounting multiple feet of the set of feet to the insulating panel at corresponding multiple corners of the insulating panel.

12. The method of claim 10 , further comprising forming the cellular structure into a honeycomb structure.

13. The method of claim 10 , further comprising forming the insulating panel with melamine.

14. The method of claim 10 , further comprising forming the cellular structure with aluminum.

15. The method of claim 10 , further comprising distributing the plurality of voids throughout the backplane in an arrangement of shapes closely fitted together in a repeated pattern without gaps or overlapping.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Aug 17, 2020
From: SMITH, MICHAEL JAMES; RAINBOW, ALEXANDER JAMES
To: GE AVIATION SYSTEMS LIMITED
Reel/Frame 053513/0692 →
Continuity (1)
Related Publication 20220048624A1 · Feb 17, 2022