Light weight housing for internal component and method of making

Patent metadata

Field	Value
Publication number	US-10323325-B2
Application number	US-201615096664-A
Country	US
Kind code	B2
Filing date	Apr 12, 2016
Priority date	Apr 12, 2016
Publication date	Jun 18, 2019
Grant date	Jun 18, 2019

Abstract

A method of making a light weight housing for an internal component is provided. The method including the steps of: forming a first metallic foam core into a desired configuration; forming a second metallic foam core into a desired configuration; inserting an internal component into the first metallic foam core; placing the second metallic foam adjacent to the first metallic core in order to secure the internal component between the first metallic foam core and the second metallic foam core; and applying an external metallic shell to an exterior surface of the first metallic foam core and the second metallic foam core.

First claim

What is claimed is:

1. A method of making a housing for an internal component to be received within the housing, comprising:
forming a first metallic foam core into a first pre-form;
forming a second metallic foam core into a second pre-form, the first pre-form being configured to mate with the second pre-form;
inserting the internal component into the first metallic foam core after it has been formed into the first pre-form, wherein the first pre-form and the second pre-form are configured to surround the internal component and wherein the internal component is a tube manifold;
placing the second pre-form adjacent to the first pre-form in order to secure the internal component between the first pre-form and the second pre-form; and
applying an external metallic shell to an exterior surface of the first pre-form and the second pre-form after placing the second pre-form adjacent to the first pre-form.

2. The method as in claim 1 , further comprising: clamping the first pre-form and the second pre-form about the tube manifold.

3. The method as in claim 1 , wherein the metal of the metallic foam cores is selected from the group comprising: titanium; cobalt; aluminum; nickel; steel alloys; magnesium; copper; molybdenum; niobium; tungsten; zinc alloys; titanium aluminide; nickel aluminide; and molybdenum disilicide.

4. The method as in claim 1 , wherein the metallic foam cores are selected from the group comprising: open cell structures and closed cell structures.

5. The method as in claim 1 , wherein the metallic foam cores are formed into the pre forms by a machining process selected from the group comprising: milling; grinding; electrical discharge machining (EDM); water-jet machining; and laser machining, wherein the pre-forms are slightly smaller than the final dimensions of the housing.

6. The method as in claim 1 , wherein the metallic foam cores each comprise a sheet of metallic foam and the sheet of metallic foam is formed into the pre-form by a hot or cold forming process wherein the sheet of metallic foam is placed in a die.

7. The method as in claim 6 , wherein the metallic foam cores are formed into the pre forms by a machining process selected from the group comprising: milling; grinding; electrical discharge machining (EDM); water-jet machining; and laser machining after the hot or cold forming process.

8. The method as in claim 1 , wherein the external metallic shell is deposited on the exterior surface of the first pre-form and the second pre-form via an application process selected from the group comprising: flame spray application process; plasma spray application process; cold-spray application process; electron beam physical vapor deposition (EB/PVD), chemical vapor deposition (CVD); and electroplating application process, and wherein the external metallic shell is deposited upon the entire exterior surface of the pre-forms.

9. The method as in claim 1 , wherein an interim coat is deposited on the exterior surface of the first pre-form and the second pre-form prior to the application of the external metallic shell.

10. The method as in claim 9 , wherein the interim coat is a ceramic based thermal barrier coating.

11. The method as in claim 1 , further comprising the step of: heat treating the first pre-form and the second pre-form after the external metallic shell has been applied to the exterior surface of the pre-forms.

12. The method as in claim 1 , further comprising the step of: forming additional features in the first pre-form and the second pre-form after the external metallic shell has been applied to the exterior surface of the pre-forms.

13. The method as in claim 12 , wherein the additional features are formed by a drilling process.

14. The method as in claim 13 , wherein a supplemental application of the external metallic outer shell is applied to the first pre-form and the second pre-form after the drilling process.

15. The method as in claim 1 , wherein a thickness of the external metallic outer shell varies in order to provide localized structural rigidity to the housing.

16. The method as in claim 1 , wherein the tube manifold is a fluid conduit.

17. A method of making a housing for an internal component to be received within the housing, comprising:
forming a first metallic foam core into a first pre-form, wherein the first pre-form has a first recessed pocket;
forming a second metallic foam core into a second pre-form, wherein the second pre-form has a second recessed pocket;
inserting the internal component into the first recessed pocket of the first pre-form after it has been formed into the first pre-form, wherein the first pre-form and the second pre-form are configured to surround the internal component and wherein the internal component is a tube manifold;
placing the second pre-form adjacent to the first pre-form, wherein the internal component is received within the first recessed pocket and the second recessed pocket and is located between the first pre-form and the second pre-form; and
applying an external metallic shell to an exterior surface of the first pre-form core and the second pre-form after placing the second pre-form adjacent to the first pre-form.

18. The method as in claim 17 , wherein the metallic foam cores are formed into the pre forms by a machining process selected from the group comprising: milling; grinding; electrical discharge machining (EDM); water jet machining; and laser machining, and wherein the external metallic shell is selectively applied to vary the thickness of the external metallic shell in order to provide localized structural rigidity to the housing.

Assignees

• United Technologies Corp

Inventors

• Roberge Gary D

Classifications

• B23K2101/18

  Sheet panels · CPC title

• B32B3/28

  characterised by a layer comprising a deformed thin sheet {, i.e. the layer having its entire thickness deformed out of the plane}, e.g. corrugated, crumpled (B32B29/08 takes precedence) · CPC title

• B23K26/36

  Removing material (B23K26/55, B23K26/57 take precedence) · CPC title

• C25D3/38

  of copper · CPC title

• B32B2255/20

  Inorganic coating · CPC title