Composite structures for storing thermal energy

• US 7,653,276 B1
• Filed: 03/06/2008
• Issued: 01/26/2010
• Est. Priority Date: 03/06/2008
• Status: Expired due to Fees

• Current Assignee: HRL Laboratories LLC (The Boeing Co.)
• Original Assignee: HRL Laboratories LLC (The Boeing Co.)
• Inventors: Jacobsen, Alan J., Gross, Adam F., Cumberland, Robert, Skeith, Sky L., Finnila, Ronald M.
• Primary Examiner(s): PENG, CHARLIE YU
• Application Number:
  US12/075,033
• Time in Patent Office: 691 Days
• Field of Search: 385/46, 385 95- 99, 385129-132
• US Class Current: 385/46
• CPC Class Codes: F28D 20/023 the latent heat storage material being enclosed in granular particles or dispersed in a porous, fibrous or cellular structure
• CPC Class Codes: Y02E 60/14 Thermal energy storage

Abstract

A composite structure for storing thermal energy. In one embodiment, an apparatus for storing thermal energy includes: a thermal storage material and a three-dimensional structure. The three-dimensional structure includes: a plurality of first truss elements defined by a plurality of first self-propagating polymer waveguides and extending along a first direction; a plurality of second truss elements defined by a plurality of second self-propagating polymer waveguides and extending along a second direction; and a plurality of third truss elements defined by a plurality of third self-propagating polymer waveguides and extending along a third direction. The first, second, and third truss elements interpenetrate each other at a plurality of nodes to form a continuous material. The first, second, and third truss elements define an open space. The thermal storage material occupies at least a portion of the open space, and the three-dimensional structure is self-supporting.

Claims

1. An apparatus for storing thermal energy, the apparatus comprising:

a thermal storage material; and

a three-dimensional structure comprising;

a plurality of first truss elements defined by a plurality of first self-propagating polymer waveguides and extending along a first direction;

a plurality of second truss elements defined by a plurality of second self-propagating polymer waveguides and extending along a second direction; and

a plurality of third truss elements defined by a plurality of third self-propagating polymer waveguides and extending along a third direction;

wherein the first, second, and third truss elements interpenetrate each other at a plurality of nodes to form a continuous material;

wherein the first, second, and third truss elements define an open space;

wherein the thermal storage material occupies at least a portion of the open space; and

wherein the three-dimensional structure is self-supporting.

2. The apparatus of claim 1, wherein at least one of the first, second, or third truss elements comprises a chemically treated surface.

3. The apparatus of claim 2, wherein the chemically treated surface comprises a material selected from the group consisting of a silane treated surface, a surfactant treated surface, and an amphoteric polymer treated surface.

4. The apparatus of claim 1, further comprising:

a metal layer coating at least one portion of at least one of the first, second, or third truss elements and adapted to change a surface polarity of the at least one portion of the at least one of the first, second, or third truss elements.

5. The apparatus of claim 4, wherein the metal layer comprises a material selected from the group consisting of nickel (Ni), copper (Cu), gold (Au), silver (Ag), ruthenium (Ru), platinum (Pt), rhodium (Rh), cobalt (Co), iron (Fe), and zinc (Zn).

6. The apparatus of claim 1, further comprising:

a ceramic layer coating at least a portion of at least one of the first, second, or third truss elements and adapted to change a surface polarity of the at least one portion of the at least one of the first, second, or third truss elements.

7. The apparatus of claim 1, wherein the ceramic layer comprises a material selected from the group consisting of silicon oxycarbide (SiOC), silicon carbide (SiC), silicon nitride (SiN), hafnium carbide (HfC), chromium carbide (CrC), boron nitride (B₄N), cubic boron nitride (c-BN), hexagonal boron nitride (h-BN), and amorphous boron nitride (α

-BN).

8. The apparatus of claim 1, wherein the thermal storage material comprises a phase change material.

9. The apparatus of claim 8, wherein the phase change material has a phase change characteristic at a temperature from about −

20°

C. to about 200°

C.

10. The apparatus of claim 1, wherein the thermal storage material comprises an organic material having a phase change characteristic at a temperature from about −

20°

C. to about 200°

C.

11. The apparatus of claim 10, wherein the organic material comprises a material selected from the group consisting of a hydrocarbon, a fatty acid, and a paraffin wax.

12. The apparatus of claim 1, wherein the thermal storage material comprises a salt hydrate having a phase change characteristic at a temperature from about 0°

C. to about 150°

C.

13. The apparatus of claim 12,

wherein the salt hydrate has a molecular formula of A^yB⁻

x.zH₂O;

wherein A is a cation having a charge of y;

wherein B is an anion having a charge of −

x; and

wherein z is an integer greater than or equal to 1.

14. The apparatus of claim 1, wherein the first, second, and third truss elements are adapted to axially transfer a mechanical load applied to the apparatus.

15. The apparatus of claim 1, wherein each of the first, second, and third truss elements has an axial diameter from about 10 μ

m to about 0.5 mm.