Carbon nanotube based heat shield

Patent metadata

Field	Value
Publication number	US-11292586-B2
Application number	US-201815979118-A
Country	US
Kind code	B2
Filing date	May 14, 2018
Priority date	May 14, 2018
Publication date	Apr 5, 2022
Grant date	Apr 5, 2022

Abstract

The present disclosure provides a heat shield. The heat shield may comprise a first layer comprising a first material, a second layer radially outward of the first layer comprising a second material, and a third layer radially outward of the second layer comprising a third material, wherein the first layer is coupled to the second layer by at least one post and at least one support extending from a radially outer surface of the first layer.

First claim

What is claimed is:

1. A heat shield comprising,
a first layer comprising a first material;
a second layer radially outward of the first layer comprising a second material;
a plurality of supports extending between and terminating at a radially outer surface of the first layer and a radially inner surface of the second layer, wherein each support is selected from the group consisting of a post or a continuous ring extending circumferentially around the first layer;
an air pocket that extends between the radially outer surface of the first layer and the radially inner surface of the second layer and between an adjacent pair of supports of the plurality of supports; and
a third layer radially outward of the second layer comprising a third material;
wherein the second material comprises a carbon nanotube sheet; and
wherein the first material and the third material are either of a first configuration or a second configuration, the first configuration being that the first material and third material comprise one of a steel or steel alloy material, the second configuration being that the first material and third material comprise a composite material.

2. A brake assembly for an aircraft comprising the heat shield of claim 1 , wherein a radially inner surface of the first layer is proximate to a brake stack and wherein a radially outer surface of the third layer is proximate to a wheel.

3. The heat shield of claim 1 , further comprising a coating surrounding at least one of the first, second, or third layers.

4. The heat shield of claim 1 , wherein each support of the plurality of supports is integral with the first layer.

5. The heat shield of claim 1 , wherein the third layer is coupled to the second layer by a second plurality of supports extending from a radially inner surface of the third layer.

6. The heat shield of claim 1 , wherein the first layer further comprises a plurality of channels on the radially outer surface of the first layer.

7. A brake assembly for an aircraft comprising, a heat shield comprising,
a first layer comprising a first material;
a second layer radially outward of the first layer comprising a second material;
a plurality of supports extending between and terminating at a radially outer surface of the first layer and a radially inner surface of the second layer, wherein each support is selected from the group consisting of a post or a continuous ring extending circumferentially around the first layer;
an air pocket that extends between the radially outer surface of the first layer and the radially inner surface of the second layer and between an adjacent pair of supports of the plurality of supports; and
a third layer radially outward of the second layer comprising a third material;
wherein the first material and third material comprise a carbon nanotube sheet and the second material comprises a steel or steel alloy material.

8. The brake assembly of claim 7 , wherein the third layer is coupled to the second layer by a second plurality of supports extending from a radially inner surface of the third layer.

9. The brake assembly of claim 7 , wherein a radially inner surface of the first layer is proximate to a brake stack and wherein a radially outer surface of the third layer is proximate to a wheel.

10. The brake assembly of claim 7 , wherein each support of the plurality of supports is integral with the first layer.

11. The brake assembly of claim 7 , wherein the first layer further comprises a plurality of channels on the radially outer surface of the first layer.

12. A heat shield comprising,
a first layer comprising a first material;
a second layer radially outward of the first layer comprising a second material;
a plurality of supports extending between and terminating at a radially outer surface of the first layer and a radially inner surface of the second layer, wherein each support is selected from the group consisting of a post or a continuous ring extending circumferentially around the first layer;
an air pocket that extends between the radially outer surface of the first layer and the radially inner surface of the second layer and between an adjacent pair of supports of the plurality of supports; and
a third layer radially outward of the second layer comprising a third material;
wherein the first material and third material comprise a first carbon nanotube sheet comprising a first density of carbon nanotube fibers and the second material comprises a second nanotube sheet comprising a second density of carbon nanotube fibers.

13. A brake assembly for an aircraft comprising the heat shield of claim 12 , wherein a radially inner surface of the first layer is proximate to a brake stack and wherein a radially outer surface of the third layer is proximate to a wheel.

14. The heat shield of claim 12 , further comprising a coating surrounding at least one of the first, second, or third layers.

15. The heat shield of claim 12 , wherein each support of the plurality of supports is integral with the first layer.

16. The heat shield of claim 12 , wherein the third layer is coupled to the second layer by a second plurality of supports extending from a radially inner surface of the third layer.

17. The heat shield of claim 12 , wherein the first layer further comprises a plurality of channels on the radially outer surface of the first layer.

Assignees

• Goodrich Corp

Inventors

• Ngatu Grum
• Voleti Sreenivasa R
• May William P
• Filburn Thomas P

Classifications

• B32B15/04 Primary

  comprising metal as the main or only constituent of a layer, {which is} next to another layer of {the same or of} a {different material (next to a bituminous or tarry layer B32B11/08; next to a water-setting substance layer B32B13/06; next to a glass layer B32B17/061; next to a cellulosic plastic layer B32B23/042)} · CPC title

• B64C25/42 Primary

  Arrangement or adaptation of brakes · CPC title

• F16D55/38

  mechanically actuated · CPC title

• F16D55/40

  actuated by a fluid-pressure device arranged in or one the brake · CPC title

• B32B2307/732

  Dimensional properties · CPC title