Low-heat-transfer interface between metal parts

Patent metadata

Field	Value
Publication number	US-9012824-B2
Application number	US-201113048942-A
Country	US
Kind code	B2
Filing date	Mar 16, 2011
Priority date	Mar 16, 2011
Publication date	Apr 21, 2015
Grant date	Apr 21, 2015

Abstract

A low-heat-transfer coupling or assembly is configured to mechanically couple together a pair of mating parts, one of which may be in a heat-producing environment. By roughening at least part of the surface of one of the parts, the contact area between the mating parts can be reduced, while still maintaining the structural integrity of the connection. The roughening can be a knurling process of all or part of the mating surface on one of the parts. This can produce a series of recesses on the surface that are in contact with the other part. The recesses can be small enough, interspersed with non-etched areas of the contact surface, that structural integrity of the coupling between the parts is still maintained. The coupling may be between a leading edge of an aircraft control surface, such as a missile fin, and a body of the control surface.

First claim

What is claimed is:

1. A low-heat-transfer assembly comprising:
a first part configured for use in a heat-producing environment; and
a second part that mates with the first part in an interference fit;
wherein the first part has a roughened surface where the first part is in contact with the second part;
wherein the roughened surface reduces contact area between the first part and the second part, relative to contact that would be produced by a smooth surface in place of the rough surface, with the roughened surface area having a contact area reduction of 40% to 80% relative to the smooth surface;
wherein the second part includes a coating on surfaces of the second part where the second part is in contact with the fist part; and
wherein the coating and second part are composed of the materials different from one another.

2. The assembly of claim 1 , wherein the roughened surface is a knurled surface.

3. The assembly of claim 1 , wherein the roughened surface is a laser etched surface.

4. The assembly of claim 1 , wherein the first part and the second part are both metal parts.

5. The assembly of claim 4 , wherein the first part includes a refractory metal or an alloy containing a refractory metal.

6. The assembly of claim 4 ,
wherein the first part is made of a material having a service temperature above 1000° C.; and
wherein the second part is made of a material having a service temperature below 1000° C.

7. The assembly of claim 1 , wherein the coating includes a ceramic material.

8. The assembly of claim 1 , wherein the coating includes at least one of silicon carbide or zirconium dioxide.

9. The assembly of claim 1 , wherein the first part includes a protrusion that is in a slot in the second part.

10. The assembly of claim 9 , wherein the roughened surface includes side surfaces of the protrusion that are engaged with side surfaces of the slot.

11. The assembly of claim 9 , wherein a gap is defined between a distal end surface of the protrusion, and a bottom surface of the slot.

12. The assembly of claim 9 ,
further comprising rivets that secure the first part and the second part together;
wherein the rivets pass through first rivet holes in the first part, and second rivet holes in the second part.

13. The assembly of claim 12 ,
wherein at least one of the first rivet holes is a substantially circular hole, and wherein other of the first rivet holes are slotted holes that have a greater extent in one direction than they do in another direction that is perpendicular to the one direction; and
wherein at least one of the second rivet holes is a substantially circular hole, and wherein other of the second rivet holes are slotted holes that have a greater extent in one direction than they do in another direction that is perpendicular to the one direction.

14. The assembly of claim 9 ,
wherein protrusion has a wedge shape, widening from a relatively narrow proximal end that is coupled to a body of the first part, to a relatively broad distal end away from the body; and
wherein the slot has a wedge shape that corresponds to the wedge shape of the protrusion.

15. The assembly of claim 1 , wherein the roughened surface area has a contact area reduction of 50% to 75% relative to the smooth surface.

16. The assembly of claim 1 ,
wherein the roughened surface includes recesses, thereby reducing the contact area between the first part and the second part, and
wherein the recesses have a depth of 0.25 mm to 2.5 mm.

17. The assembly of claim 1 , wherein the coating has a thickness of 0.025 mm to 0.05 mm.

18. A missile control surface assembly comprising:
a refractory-metal-containing leading edge; and
a metal main body coupled to the leading edge;
wherein the refractory-metal-containing leading edge has roughened surfaces that are in contact with coated surfaces of the main body;
wherein the coated surfaces are composed of a material different from the metal main body; and
wherein the roughened surfaces reduce contact area between the leading edge and the main body, relative to contact that would be produced by smooth surfaces in place of the rough surfaces, with the roughened surfaces area having a contact area reduction of 40% to 80% relative to the smooth surfaces.

19. A low-heat-transfer assembly comprising:
a first part configured for use in a heat-producing environment; and
a second part that mates with the first part in an interference fit;
wherein the first part has a roughened surface where the first part is in contact with the second part;
wherein the roughened surface reduces contact area between the first part and the second part, relative to contact that would be produced by a smooth surface in place of the roughened surface, with the roughened surface area having a contact area reduction of 40% to 80% relative to the smooth surface; and
wherein the first part includes a protrusion that is in a slot in the second part; and
further comprising rivets that secure the first part and the second part together, wherein the rivets pass through first rivet holes in the first part, and through second rivet holes in the second part.

20. The assembly of claim 19 ,
wherein at least one of the first rivet holes in a substantially circular hole, and wherein other of the first rivet holes are slotted holes that have a greater extent in one direction than they do in another direction that is perpendicular to the one direction; and
wherein at least one of the second rivet holes is a substantially circular hole, and wherein other of the second rivet holes are slotted holes that have a greater extent in one direction than they do in another direction that is perpendicular to the one direction.

Assignees

• Christou Kyriakos C
• Raytheon Co

Inventors

• Christou Kyriakos C

Classifications

• Y10T29/49826

  Assembling or joining · CPC title

• F05D2250/60

  Structure; Surface texture · CPC title

• F01D25/00 Primary

  Component parts, details, or accessories, not provided for in, or of interest apart from, other groups · CPC title

• F42B10/64

  of fins · CPC title

• F42B10/06

  Tail fins · CPC title