Heat-managing composite structures

Patent metadata

Field	Value
Publication number	US-9920530-B2
Application number	US-59654808-A
Country	US
Kind code	B2
Filing date	Apr 17, 2008
Priority date	Apr 17, 2007
Publication date	Mar 20, 2018
Grant date	Mar 20, 2018

Abstract

Light-weight, heat-managing structures feature open-cell lattice, honeycomb, and/or corrugated (prismatic) arrangements in their substructures, combined with heat pipe/heat plate arrangements for managing heat to which the structures are subjected. The structures are well suited to aerospace applications and may be employed in the leading edge of wings or other airfoil-shaped components; gas turbine engine components; rocket nozzles; and other high-heat, high-stress environments.

First claim

We claim:

1. A structural arrangement, comprising:
an open-cell lattice-structure core;
a surface layer comprising a cellular sub-structure; and
a heat-transferring working fluid disposed within said core or said surface layer;
wherein the surface layer further comprises an outer arrangement that has lower thermal conductivity than the cellular sub-structure of said surface layer.

2. The structural arrangement of claim 1 , wherein a heat-transferring working fluid is disposed within each of said core and said surface layers.

3. The structural arrangement of claim 1 , wherein the lattice structure of said core is selected from the group consisting of tetrahedral, pyramidal, three-dimensional Kagome; diamond or textile weave; square, collinear hollow truss; and diamond, collinear hollow truss structural arrangements.

4. The structural arrangement of claim 1 , wherein the lattice structure of said core is formed from solid struts.

5. The structural arrangement of claim 4 , wherein said heat-transferring working fluid is present in wicking material disposed within the interstices of the lattice structure of said core.

6. The structural arrangement of claim 1 , wherein the lattice structure of said core is formed from hollow struts.

7. The structural arrangement of claim 6 , wherein said heat-transferring working fluid is disposed within said hollow struts in a manner such that the hollow struts function as heat pipes.

8. The structural arrangement of claim 7 , wherein said heat-transferring working fluid is present in wicking material disposed within said hollow struts.

9. The structural arrangement of claim 1 , wherein the cellular sub-structure of said surface layer is an open-cell lattice structure.

10. The structural arrangement of claim 9 , wherein the open-cell lattice structure of said surface layer is selected from the group consisting of tetrahedral, pyramidal, three-dimensional Kagome; diamond or textile weave; square, collinear hollow truss; and diamond, collinear hollow truss structural arrangements.

11. The structural arrangement of claim 1 , wherein said heat-transferring working fluid is disposed within interstices of the cellular sub-structure of the surface layer.

12. The structural arrangement of claim 1 , wherein the outer arrangement consists of a thermal barrier coating.

13. The structural arrangement of claim 1 , wherein the cellular sub-structure of the surface layer is fabricated from carbon/carbon, silicon-carbon/silicon-carbon, or intermetallic material.

14. The structural arrangement of claim 1 , wherein said arrangement is incorporated in the leading edge of a wing or other airfoil-shaped body.

15. The structural arrangement of claim 1 , wherein said arrangement is incorporated in a component of a gas turbine engine.

16. The structural arrangement of claim 15 , wherein said component is a stator or rotor blade.

17. A structural arrangement, comprising:
a substrate; and
an outermost face layer spaced from and joined to the substrate by means of a cellular structure, the outermost face layer being fabricated from a material having a thermal conductivity that is lower than a thermal conductivity of said cellular structure.

18. The structural arrangement of claim 17 , wherein the outermost face layer is fabricated from fiber-reinforced, ceramic matrix composite; thermal barrier composition; or a closed cell structure made from a material having a thermal conductivity that is lower than a thermal conductivity of said cellular structure.

19. The structural arrangement of claim 17 , wherein the cellular structure comprises an open-cell lattice structure.

20. The structural arrangement of claim 19 , wherein the open-cell lattice structure is selected from the group consisting of tetrahedral, pyramidal, three-dimensional Kagome; diamond or textile weave; square, collinear hollow truss; and diamond, collinear hollow truss structural arrangements.

21. The structural arrangement of claim 19 , wherein the lattice structure is formed from solid struts.

22. The structural arrangement of claim 19 , wherein the lattice structure is formed from hollow struts.

23. The structural arrangement of claim 22 , wherein the hollow struts are filled with heat-transferring working fluid.

24. The structural arrangement of claim 23 , further comprising wicking material disposed within said hollow struts.

25. The structural arrangement of claim 17 , wherein the cellular structure is a corrugated or prismatic structure.

26. The structural arrangement of claim 25 , wherein the corrugated or prismatic structure is selected from the group consisting of triangular, diamond, and Navtruss® corrugation arrangements.

27. The structural arrangement of claim 17 , wherein portions of said cellular structure are embedded within the outermost face layer.

28. The structural arrangement of claim 17 , wherein said cellular structure is diffusion bonded, brazed, or welded to said substrate.

29. The structural arrangement of claim 17 , further comprising a phase change material disposed within interstices of the cellular structure.

Assignees

• Wadley Haydn N G
• Queheillalt Douglas T
• Univ Virginia Patent Foundation

Inventors

• Wadley Haydn N G
• Queheillalt Douglas T

Classifications

• E04C2/34 Primary

  composed of two or more spaced sheet-like parts (E04C2/32 takes precedence; spacers for cavity walls E04B2/44) · CPC title

• E04C2002/345

  with triangular corrugations · CPC title

• E04C2/3405

  spaced apart by profiled spacer sheets · CPC title

• E04C2002/3488

  spaced apart by frame like structures · CPC title

• E04C2/365

  by honeycomb structures · CPC title