High aspect ratio, microstructure-covered, macroscopic surfaces

• US 5,681,661 A
• Filed: 02/09/1996
• Issued: 10/28/1997
• Est. Priority Date: 02/09/1996
• Status: Expired due to Fees

• Current Assignee: Board of Supervisors of Louisiana State University Agricultural & Mechanical College (Louisiana State University System)
• Original Assignee: Board of Supervisors of Louisiana State University Agricultural & Mechanical College (Louisiana State University System)
• Inventors: Kelly, Kevin W.
• Primary Examiner(s): ZIMMERMAN, JOHN J
• Application Number:
  US08/599,151
• Time in Patent Office: 627 Days
• Field of Search: 428/687, 428/612, 428/601, 428/610, 428/609, 416/241 R, 416/241 B, 416/235, 416/236 R, 181/293, 181/294, 181/286, 165/133, 165/DIG. 515
• US Class Current: 428/601
• CPC Class Codes: B01J 19/0093 Microreactors, e.g. miniaturised or microfabricated reactors laboratory containers with capillary fluid transport in microfabricated channels or chambers B01L3/5027
• CPC Class Codes: C25D 5/022 using masking means
• CPC Class Codes: F28F 13/18 by applying coatings, e.g. radiation-absorbing, radiation-reflecting; by surface treatment, e.g. polishing
• CPC Class Codes: F28F 2260/02 having microchannels
• CPC Class Codes: Y10T 428/12396 Discontinuous surface component
• CPC Class Codes: Y10T 428/12458 having composition, density, or hardness gradient
• CPC Class Codes: Y10T 428/12472 Microscopic interfacial wave or roughness
• CPC Class Codes: Y10T 428/12993 Surface feature [e.g., rough, mirror]

Abstract

The performance of many macroscopic structures (those whose dimensions are on the order of centimeters, meters, or even larger) can be greatly improved by covering their surfaces with microstuctures. There are several applications in which "large," microstructure-covered sheets are useful. For example, dissimilar sheets of material that otherwise would not bond well to one another (such as a polymer and a metal) can be more strongly bonded with microstructures extending from one of the sheets and embedded into the other sheet. Such products make valuable laminate composites. As another example, the rate of heat transfer between an object and the surrounding medium can be dramatically changed (up or down) by covering the surface of the object with high aspect ratio microstructures, without significantly changing the component'"'"'s size or weight. As compared to prior thermal barrier coatings, when microstructures are thus used to cover turbine blades the turbines can operate at substantially higher temperatures (as much as 290° C. higher than otherwise possible) and substantially higher pressures, while simultaneously reducing thermal stresses. Yet another application is the use of microstructures as acoustic absorbers, to reduce the amplitude of sound transmitted through a surface.

Claims

1. An article of manufacture comprising a heat barrier to reduce heat transfer between an object and the surroundings, wherein:

(a) the object has a first face whose surface area is at least about 10 cm² ;

(b) said heat barrier comprises a plurality of at least about 10 microstructures per cm² of surface area of the first face;

(c) each of said microstructures comprises a shield and a post, wherein each of said shields comprises a distal face and a proximal face, and wherein each of said posts comprises a distal end and a proximal end;

(d) said distal end of said post of each of said microstructures is connected to said proximal face of said shield of said microstructure;

(e) said proximal end of said post of each of said microstructures is connected to the first face of the object;

(f) the surface area of the distal face of each of said shields is at least about 0.001 mm² ; and

(g) the distance between the proximal face of each of said shields and the first face of the object is between about 0.01 mm and about 2.0 mm;

whereby total heat transfer between the object and the surroundings is substantially less than would be the heat transfer between an otherwise identical object lacking said heat barrier and the surroundings.

2. An article of manufacture as recited in claim 1, wherein:

(a) said heat barrier comprises a plurality of at least about 5000 microstructures per cm² of surface area of the first face;

(b) the surface area of the distal face of each of said shields is at least about 0.01 mm² ; and

(c) the distance between the proximal face of each of said shields and the first face of the object is between about 0.1 mm and about 1.0 mm.

3. An article of manufacture as recited in claim 1, wherein the object comprises a turbine blade.

4. An article of manufacture as recited in claim 3, wherein said turbine blade comprises a nickel alloy;

and wherein each of said shields comprises a composition selected from the group consisting of Al₂ O₃, Cr₂ O₃, a Ni--Al binary alloy, a Ni--Cr--Al ternary alloy, and a Ni--Cr--Al--Y quaternary alloy.

5. An article of manufacture as recited in claim 4, wherein the composition of each of said posts comprises a gradient wherein the composition of the proximal end of said post is substantially identical to the composition of said turbine blade, and wherein the composition of the distal end of said post is substantially identical to the composition of said shields.

6. An article of manufacture comprising a heat barrier to reduce heat transfer between an object and the surroundings, wherein:

(a) the object has a first face whose surface area is at least about 10 cm² ;

(b) said heat barrier comprises a substantially continuous layer that is substantially parallel to said first face, and that is connected to said first face by a plurality of at least about 10 microstructures per cm² of surface area of the first face;

(c) each of said microstructures comprises a distal end and a proximal end;

(d) said distal end of each of said microstructures is connected to said substantially continuous layer;

(e) said proximal end of each of said microstructures is connected to the first face of the object; and

(f) the distance between said substantially continuous layer and the first face of the object is between about 0.01 mm and about 2.0 mm;

whereby total heat transfer between the object and the surroundings is substantially less than would be the heat transfer between an otherwise identical object lacking said heat barrier and the surroundings.

7. An article of manufacture as recited in claim 6, wherein the distance between said substantially continuous layer and the first face of the object is between about 0.1 mm and about 1.0 mm.

8. An article of manufacture as recited in claim 6, wherein the object comprises a turbine blade.

9. An article of manufacture as recited in claim 8, wherein said turbine blade comprises a nickel alloy;

and wherein said substantially continuous layer comprises a composition selected from the group consisting of Al₂ O₃, Cr₂ O₃, a Ni--Al binary alloy, a Ni--Cr--Al ternary alloy, and a Ni--Cr--Al--Y quaternary alloy.

10. An article of manufacture as recited in claim 9, wherein the composition of each of said posts comprises a gradient wherein the composition of the proximal end of said post is substantially identical to the composition of said turbine blade, and wherein the composition of the distal end of said post is substantially identical to the composition of said substantially continuous layer.

11. An article of manufacture comprising a heat barrier to reduce heat transfer between an object and the surroundings, wherein:

(a) the object has a face whose surface area is at least about 10 cm² ;

(b) said heat barrier comprises a plurality of at least about 10 microstructures connected to said first face, wherein adjacent microstructures are spaced between about 10 μ

m and about 500 μ

m apart from one another; and

(c) each of said microstructures comprises a wall substantially perpendicular to said face, to partially enclose and thereby inhibit heat transfer near said face, wherein said wall is at least about 0.1 mm tall in the direction perpendicular to said face, and wherein the height of said microstructures is at least about 5 times the distance between adjacent microstructures;

whereby total heat transfer between the object and the surroundings is substantially less than would be the heat transfer between an otherwise identical object lacking said heat barrier and the surroundings.

12. An article of manufacture as recited in claim 11, where adjacent microstructures are spaced between about 20 μ

m and about 50 μ

m apart from one another;

wherein said wail is at least about 0.5 mm tall in the direction perpendicular to said face; and

wherein the height of said microstructures is at least about 10 times the distance between adjacent microstructures.

13. An article of manufacture as recited in claim 11, wherein the object comprises a turbine blade.

14. An article of manufacture comprising a heat sink to augment heat transfer between an object and the surroundings, wherein:

(a) the object has a face whose surface area is at least about 1 cm² ;

(b) said heat sink comprises a plurality of at least about 1000 microposts per cm² of surface area of the face, wherein each of said microposts has a distal end and a proximal end;

(c) said proximal end of each of said microposts is connected to the face;

(d) said distal end of each of said microposts is not connected to a shield, wall, or other object that inhibits heat transfer; and

(e) the distance between the proximal and distal ends of each of said microposts is between about 0.05 mm and about 1.0 mm, and the aspect ratio of each of said microposts is at least about 5;

wherein the aspect ratio of a micropost is the ratio of the distance between the proximal end and the distal end of the micropost to the characteristic dimension of the micropost;

wherein the characteristic dimension of a micropost is the diameter of the micropost in a plane perpendicular to a line between the proximal end and the distal end of the micropost;

whereby total heat transfer between the object and the surroundings is substantially greater than would be the heat transfer between an otherwise identical object lacking said microposts and the surroundings.

15. An article of manufacture as recited in claim 14, wherein:

(a) said heat sink comprises a plurality of at least about 10,000 microstructures per cm² of surface area of the face;

(b) the distance between the proximal and distal ends of each of said microposts is at least about 0.1 mm; and

(c) each said micropost is farther from the nearest neighboring micropost than a distance of about 5 times the diameter of said micropost.

16. A composite material comprising a first layer of a first substance, and a second layer of a second substance that is different from the first substance, wherein:

(a) each of said layers comprises a proximal face, and the proximal faces of said first and second layers are substantially in contact with one another;

(b) said proximal face of said first layer is connected to the proximal ends of each of a plurality of at least about 10 microstructures per cm² of surface area of the proximal face of said first layer, wherein each of said microstructures comprises a proximal end and a distal end;

(c) the distance between the proximal and distal ends of each of said microstructures is between about 0.01 mm and about 0.5 mm, and the aspect ratio of each of said microstructures is at least about 5;

wherein the aspect ratio of a microstructure is the ratio of the distance between the proximal end and the distal end of the microstructure to the characteristic dimension of the microstructure;

wherein the characteristic dimension of a microstructure is the diameter of the microstructure in a plane perpendicular to a line between the proximal end and the distal end of the microstructure; and

(d) the shape of said proximal face of said second layer is substantially complementary to said microstructures;

whereby the adhesion between said first and second layers is substantially greater than would be the adhesion between two otherwise identical layers lacking said microstructures.

17. A composite material as recited in claim 16, wherein:

(a) said proximal face of said first layer is connected to the proximal ends of each of a plurality of at least about 100 microstructures per cm² of surface area of the proximal face of said first layer;

(b) the distance between the proximal and distal ends of each of said microstructures is between about 0.1 mm and about 0.5 mm, and the aspect ratio of each of said microstructures is at least about 10; and

(c) each of said microstructures is closer to the nearest neighboring microstructure than a distance of about 5 times the width of said microstructure.

18. A composite material as recited in claim 16, wherein the shape of said microstructures is such that said microstructures are physically interlocked securely with said second layer, even disregarding any chemical bonding that may exist between said microstructures and said second layer.

19. An article of manufacture comprising an acoustic barrier to reduce transmission of sound having a frequency above a characteristic frequency through an object, wherein:

(a) the object has a first face whose surface area is at least about 10 cm² ;

(b) said acoustic barrier comprises a plurality of at least about 50 microstructures per cm² of surface area of the first face, wherein said microstructures are connected to the first face;

(c) each of said microstructures has a natural vibrational frequency below the characteristic frequency;

whereby transmission of sound above the characteristic frequency through the object is substantially less than would be the transmission of sound through an otherwise identical object lacking said acoustic barrier.

20. An article of manufacture as recited in claim 19, wherein said acoustic barrier comprises a plurality of at least about 500 microstructures per cm² of surface area of the first face.