Light weight component with acoustic attenuation and method of making

Patent metadata

Field	Value
Publication number	US-10302017-B2
Application number	US-201615096619-A
Country	US
Kind code	B2
Filing date	Apr 12, 2016
Priority date	Apr 12, 2016
Publication date	May 28, 2019
Grant date	May 28, 2019

Abstract

A method of making a light weight component is provided. The method including the steps of: forming a metallic foam core into a desired configuration; applying an external metallic shell to an exterior surface of the metallic foam core after it has been formed into the desired configuration; and attenuating the component to a desired frequency by forming a plurality of openings in the external metallic shell.

First claim

What is claimed is:

1. A method of making a light weight component, comprising:
forming a metallic foam core into a first configuration;
applying an external metallic shell to an exterior surface of the metallic foam core after it has been formed into the first configuration via a spray application process; and
attenuating the component to a frequency by forming a plurality of openings in the external metallic shell.

2. The method as in claim 1 , wherein the plurality of openings are only located on a single side of the component.

3. The method as in claim 1 , further comprising forming a plurality of resonant chambers in the metallic foam core prior to the application of the external metallic shell, wherein at least some of the plurality of openings are in fluid communication with a respective one of the plurality of resonant chambers.

4. The method as in claim 3 , wherein the plurality of openings are located on opposite sides of the component.

5. The method as in claim 3 , wherein the metal of the metallic foam core 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 and wherein the attenuating step further comprises modifying a diameter of the plurality of openings and a size of the resonant chamber based upon a density of the metallic foam core and a thickness of the component.

6. The method as in claim 1 , wherein the plurality of openings are located on opposite sides of the component.

7. The method as in claim 1 , wherein the component is configured for use in a gas turbine engine.

8. The method as in claim 1 , wherein the metallic foam core is an open cell structure and wherein the metallic foam core comprises a plurality of separate foam cores secured to each other.

9. The method as in claim 1 , wherein the metallic foam core is formed into the first configuration by a machining process selected from the group comprising: milling; electrical discharge machining (EDM); water jet machining; and laser machining, wherein the first configuration is smaller than the final dimensions of the light weight component.

10. The method as in claim 1 , wherein the metallic foam core is a sheet of metallic foam and the sheet of metallic foam is formed into the first configuration by a hot or cold forming process wherein the sheet of metallic foam is placed in a die.

11. The method as in claim 10 , wherein the metallic foam core is formed into the first configuration 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.

12. The method as in claim 1 , wherein the spray application process is selected from the group comprising: flame spray application process; plasma spray application process; and cold-spray application process.

13. The method as in claim 1 , further comprising the step of: forming additional features in the metallic foam core after the external metallic shell has been applied to the exterior surface of the metallic foam core.

14. 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 component.

15. A component formed by the method of claim 1 , wherein the component is a portion of a tailcone of a gas turbine engine.

16. A method of making a light weight component, comprising:
forming a metallic foam core into a first configuration;
applying an external metallic shell to an exterior surface of the metallic foam core after it has been formed into the first configuration
heat treating the metallic foam core after the external metallic shell has been applied to the exterior surface of the metallic foam core; and
attenuating the component to a frequency by forming a plurality of openings in the external metallic shell.

17. The method as in claim 16 , 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 component.

18. The method as in claim 17 , further comprising forming a plurality of resonant chambers in the metallic foam core prior to the application of the external metallic shell, wherein at least some of the plurality of openings are in fluid communication with a respective one of the plurality of resonant chambers and wherein the external metallic shell is deposited on the exterior surface of the metallic foam core 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.

19. The method as in claim 18 , wherein the plurality of openings are located on opposite sides of the component.

20. A component, comprising:
a metallic foam core having a first configuration, wherein the metallic foam core is an open cell structure and wherein the metallic foam core comprises a plurality of separate foam cores secured to each other;
an external metallic shell applied to an exterior surface of the metallic foam core after it has been placed into the first configuration, wherein a thickness of the external metallic shell varies in order to provide localized structural rigidity to the component;
a plurality of resonant chambers located within the metallic foam core; and
a plurality of openings extending through a surface of the external metallic shell, wherein a portion of the plurality of openings are in fluid communication with a respective one of the plurality of resonant chambers.

Assignees

• United Technologies Corp

Inventors

• Roberge Gary D

Classifications

• B32B2266/08

  Closed cell foam · CPC title

• B32B5/32

  at least two} layers being foamed {and next to each other · CPC title

• F02K1/04

  Mounting of an exhaust cone in the jet pipe · CPC title

• B32B2266/04

  Inorganic · CPC title

• B32B3/30

  characterised by a layer formed with recesses or projections, e.g. {hollows, grooves, protuberances, ribs (apertured layer B32B3/266; layer with cavities or internal voids B32B3/26)} · CPC title