Tuned multilayered material systems and methods for manufacturing

Patent metadata

Field	Value
Publication number	US-11969796-B2
Application number	US-202016733390-A
Country	US
Kind code	B2
Filing date	Jan 3, 2020
Priority date	Jan 3, 2020
Publication date	Apr 30, 2024
Grant date	Apr 30, 2024

Abstract

A graded multilayered composite comprises a metal matrix material having a first side and a second side opposite the first side. A first layer of microspheres is dispersed on the first side of the metal matrix material. A second layer of microspheres is dispersed on the second side of the metal matrix material.

First claim

What is claimed is:

1. A graded multilayered composite, comprising:
a sintered metal matrix material, having a first edge on a first side of the sintered metal matrix material and a second edge on a second side of the sintered metal matrix material, opposite the first side, the sintered metal matrix material having a sintered metal matrix throughout the sintered metal matrix material from the first edge to the second edge;
a first layer of hollow microspheres, located on the first side of the sintered metal matrix material;
a second layer of hollow microspheres, located on the second side of the sintered metal matrix material; and
one or more cooling channels in the sintered metal matrix material between the first edge and the second edge,
wherein:
hollow microspheres of the first layer of hollow microspheres are spatially distributed relative to each other according to a first spatial gradation, each hollow microsphere having a void therein defining a void volume,
hollow microspheres of the second layer of hollow microspheres are spatially distributed relative to each other according to a second spatial gradation, each hollow microsphere having a void therein defining a void volume,
the first spatial gradation is based upon one of a number of the hollow microspheres in the first layer of hollow microspheres or a size of the hollow microspheres in the first layer of hollow microspheres, and
the second spatial gradation is based upon one of a number of the hollow microspheres in the second layer of hollow microspheres or a size of the hollow microspheres in the second layer of hollow microspheres,

wherein a total void volume fraction of the second layer is less than a total void volume fraction of the first layer.

2. The graded multilayered composite of claim 1 , wherein the second spatial gradation is different from the first spatial gradation.

3. The graded multilayered composite of claim 1 , further comprising:
a first buffer region defined between the first layer of hollow microspheres and the first edge on the first side of the sintered metal matrix material; and
a second buffer region, defined between the second layer of hollow microspheres and the second edge on the second side of the sintered metal matrix material; and
wherein each of the first buffer region and the second buffer region is substantially devoid of hollow microspheres.

4. The graded multilayered composite of claim 1 , wherein the first spatial gradation is based upon the number of the hollow microspheres in the first layer of hollow microspheres, and the second spatial gradation is based upon the number of the hollow microspheres in the second layer of hollow microspheres.

5. The graded multilayered composite of claim 1 , wherein the first spatial gradation is based upon the size of the hollow microspheres in the first layer of hollow microspheres, and the second spatial gradation is based upon the size of the hollow microspheres in the second layer of hollow microspheres.

6. The graded multilayered composite of claim 1 , wherein the hollow microspheres of the first layer of hollow microspheres and the hollow microspheres of the second layer of hollow microspheres comprise a ceramic material.

7. The graded multilayered composite of claim 1 , wherein the hollow microspheres of the first layer of hollow microspheres and the hollow microspheres of the second layer of hollow microspheres comprise at least one of yttria-stabilized zirconia and alumina-silica-iron glass.

8. The graded multilayered composite of claim 1 , wherein at least one of the hollow microspheres of the first layer of hollow microspheres and at least one of the hollow microspheres of the second layer of hollow microspheres is between 5 microns and 500 microns in diameter.

9. The graded multilayered composite of claim 1 , wherein each of the hollow microspheres of the first layer of hollow microspheres and each of the hollow microspheres of the second layer of hollow microspheres has a diameter and an average wall thickness between 2 percent and 30 percent of the diameter.

10. The graded multilayered composite of claim 1 , wherein the sintered metal matrix material comprises a compositionally graded material.

11. The graded multilayered composite of claim 10 , wherein a composition of the sintered metal matrix material comprises at least one of aluminum, aluminum alloy, aluminum metal matrix composite, titanium, titanium alloy, titanium metal matrix composite, iron, iron alloy, iron metal matrix composite, nickel, nickel alloy, nickel metal matrix composite, cobalt, cobalt alloy, cobalt metal matrix composite, a refractory metal, a refractory metal alloy, a refractory metal matrix composite, copper, a copper alloy, copper metal matrix composite, a precious metal, a precious metal alloy, a precious metal matrix composite, zirconium, a zirconium alloy, zirconium metal matrix composite, hafnium, a hafnium alloy, and hafnium metal matrix composite.

12. The graded multilayered composite of claim 1 , wherein a density of a first portion of the graded multilayered composite is different from a density of a second portion of the graded multilayered composite, wherein the sintered metal matrix material comprises a compositionally graded material, wherein the hollow microspheres of the first layer of hollow microspheres are spatially distributed relative to each other, wherein the hollow microspheres of the second layer of hollow microspheres are spatially distributed relative to each other, and wherein a distribution of the hollow microspheres of the first layer of hollow microspheres is different than a distribution of the hollow microspheres of the second layer of hollow microspheres.

13. The graded multilayered composite of claim 12 , further comprising:
a first buffer region defined between the first layer of hollow microspheres and the first edge on the first side of the sintered metal matrix material; and
a second buffer region defined between the second layer of hollow microspheres and the second edge on the second side of the sintered metal matrix material;
wherein each of the first buffer region and the second buffer region is substantially devoid of hollow microspheres.

14. A multilayered material system comprising:
the graded multilayered composite of claim 1 ; and
a layer, joined to the graded multilayered composite and selected from a monolithic or graded metallic liner, a monolithic or graded ceramic, a monolithic or graded metallic-ceramic hybrid liner, a monolithic or graded metallic core, a monolithic or graded cooling channel structure, or a monolithic or graded environmental barrier coating.

15. A method for manufacturing the multilayered material system of claim 11 , the method comprising:
joining the layer to the graded multilayered composite to provide the multilayered material system.

16. A graded multilayered composite, comprising:
a sintered metal matrix material, having a first edge on a first side of the sintered metal matrix material and a second edge on a second side of the sintered metal matrix material, opposite the first side, the sintered metal matrix material having a sintered metal matrix throughout the sintered metal matrix material from the first edge to the second edge, the sintered metal matrix material comprising a compositionally graded material;
a first layer of hollow microspheres, located on the first side of the sintered metal matrix material, each hollow microsphere having a void therein defining a void volume; and
a second layer of hollow microspheres, located on the second side of the sintered metal matri

Assignees

• Boeing Co

Inventors

• Yousefiani Ali

Classifications

• B64C1/00 Primary

  Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like · CPC title

• B32B9/005

  comprising one layer of ceramic material, e.g. porcelain, ceramic tile (layered products with at least two ceramic layers composed mainly of ceramic B32B18/00) · CPC title

• B32B15/043

  of metal (B32B15/01 takes precedence) · CPC title

• B32B3/12

  characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure · CPC title

• B22F3/1112 Primary

  comprising hollow spheres or hollow fibres · CPC title