IP Library › Granted Patent US 10,408,544
Granted Patent B2
US 10,408,544 · App. 14/282,370 · Granted Sep 10, 2019

Composite top case with embedded heat pipes

Inventors: Doug Mueller (Coppell, TX); Brian S. Modrzejewski (Keller, TX); Brad Ekstrom (Fort Worth, TX); Scott Gardner (Hurst, TX); David Elliott (Azle, TX)
F28D15/02B64C27/04B64D33/10F28D15/0275
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 10,408,544
App. No.
14/282,370
Granted
Sep 10, 2019
Kind
B2
Abstract

A system and method to transfer heat energy through a composite structure. The system includes a heat pipe extending through a thickness of the composite material. The method includes extending a heat pipe through the composite material from a first surface exposed to the heat energy to a second surface exposed to airflow.

Claims (40)

1. A cooling system for a structure composed of composite material, comprising:

a heat pipe extending through a thickness of the composite material from an inner surface of the thickness exposed to a heat energy to an outer surface of the thickness exposed to an airflow; and

an elongated bar attached to the heat pipe at a first end;

wherein the heat pipe is surrounded by the composite material about an entire outer circumference of the heat pipe along a portion of the heat pipe between the inner surface and the outer surface;

wherein the elongated bar is secured to and upon the inner surface;

wherein the heat pipe contacts the composite material;

wherein the heat pipe is configured to transfer heat energy from an inner surface of the structure susceptible to heat energy buildup to an exposed surface in contact with airflow; and

wherein the heat pipe is embedded in the composite material.

2. The system of claim 1 , wherein the elongated bar is annular along the inner surface.

3. The system of claim 1 , further comprising:

a plurality of fins secured to a second end of the heat pipe;

wherein the plurality of fins are exposed to the airflow.

4. The system of claim 1 , further comprising:

a base secured to an outer surface of the structure and attached the heat pipe;

wherein the base is exposed to the airflow.

5. The system of claim 4 , further comprising:

a plurality of fins secured to and extending from the base.

6. The system of claim 5 , further comprising:

a second base secured to the inner surface of the structure and attached to the heat pipe.

7. The system of claim 6 , further comprising:

a plurality of fins secured to and extending from the second base.

8. The system of claim 1 , further comprising:

a shaft attached to the heat pipe and extending from the inner surface of the structure.

9. The system of claim 8 , further comprising:

a plurality of fins secured to the shaft.

10. The system of claim 9 , further comprising:

a plurality of fins secured to an end of the heat pipe;

wherein the plurality of fins are exposed to the airstream.

11. The system of claim 1 , wherein the heat pipe is hollow.

12. The system of claim 11 , wherein the heat pipe houses an inert gas.

13. The system of claim 11 , wherein the heat pipe houses water vapor.

14. A method to transfer heat energy through a composite structure, comprising:

extending a heat pipe through a thickness of the composite material from an inner surface of the thickness exposed to the heat energy to an outer surface of the thickness exposed to airflow;

wherein the heat pipe is embedded in the composite structure between the inner surface and the outer surface;

wherein the heat pipe is surrounded by the composite material about an entire outer circumference of the heat pipe along a portion of the heat pipe between the inner surface and the outer surface; and

wherein the heat pipe is in contact with the composite material.

15. The method of claim 14 , further comprising:

further transferring the heat energy by securing a plurality of fins to the heat pipe.

16. The method of claim 14 , wherein the composite material is thermally non-conductive.

17. The system of claim 1 , wherein the composite material is thermally non-conductive.

Assignments (1)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 21, 2014
From: MUELLER, DOUG; MODRZEJEWSKI, BRIAN S.; EKSTROM, BRAD; GARDNER, SCOTT; ELLIOTT, DAVID
To: BELL HELICOPTER TEXTRON INC.
Reel/Frame 032943/0934 →
Continuity (1)
Related Publication 20150338170A1 · Nov 26, 2015