In-situ selective reinforcement of near-net-shaped formed structures

Patent metadata

Field	Value
Publication number	US-11052458-B2
Application number	US-201615040528-A
Country	US
Kind code	B2
Filing date	Feb 10, 2016
Priority date	Feb 10, 2015
Publication date	Jul 6, 2021
Grant date	Jul 6, 2021

Abstract

Various embodiments provide methods in which a metal matrix composite (MMC) material is incorporated into a metallic structure during a one-step near-net-shape structural forming process. Various embodiments provide in-situ selective reinforcement processes in which the MMC may be pre-placed on a forming tool in locations that correspond to specific regions in the metallic structure. Various embodiment near-net-shape structural forming processes may then be executed and result in various embodiment metallic structural components with selectively-reinforced regions that provide enhanced mechanical properties in key locations.

First claim

What is claimed is:

1. A method of in-situ selective reinforcement, comprising:
selecting at least one location of a final structural component for reinforcement;
placing a metal matrix composite (MMC) material in a forming tool in at least one location of the forming tool corresponding to the at least one location of the final structural component for reinforcement; and
forming, from a starting stock material, the final structural component using the forming tool with the MMC material placed in it, wherein the forming includes inducing plastic deformation of the stock material, and wherein the forming comprises a one-step near-net-shape structural forming process that includes spin forming using a spinning mandrel and a series of rollers to shape the final structural component
wherein the one-step near-net-shape structural forming process comprises and bonding the MMC material in-situ to a surface of the final structural component.

2. The method of claim 1 , wherein the MMC material comprises a ceramic.

3. The method of claim 1 , wherein the MMC material comprises one or more of aluminum, an aluminum alloy, alumina, and silicon-carbide.

4. The method of claim 3 , wherein the MMC material is reinforced with one or more of fibers, whiskers, or particles.

5. The method of claim 4 , wherein the MMC material is in the form of a tape.

6. The method of claim 5 , wherein the MMC material is a fiber-reinforced aluminum material including an aluminum Al-1100 alloy matrix reinforced with 50 volume percent continuous alumina fibers.

7. The method of claim 5 , wherein the MMC material is an aluminum alloy with a percent weight copper.

8. The method of claim 7 , wherein the percent weight copper is 2 percent.

9. The method of claim 5 , wherein a thickness of the tape is from 0.018 inches to 0.180 inches.

10. The method of claim 9 , wherein a width of the tape is from 0.375 inches to 0.48 inches.

11. The method of claim 1 , wherein the starting stock material is an aluminum-lithium alloy.

12. The method of claim 1 , the starting stock material comprises aluminum or an aluminum alloy.

13. The method of claim 1 , wherein the spinning mandrel comprises a cylindrical mandrel with a plurality of grooves formed on a surface thereof, and wherein the at least one location of the forming tool includes at least one surface of the plurality of grooves.

14. The method of claim 13 , wherein:
the MMC material comprises aluminum or an aluminum alloy; and
the final structural component comprises an aluminum alloy cylinder having one or more stiffeners with the MMC material bonded to a top of each of the one or more stiffeners.

15. A method of in-situ selective reinforcement, comprising:
selecting at least one location of a final structural component for reinforcement;
placing a metal matrix composite (MMC) material in a forming tool in at least one location of the forming tool corresponding to the selected at least one location of the final structural component for reinforcement, wherein the MMC material comprises aluminum or an aluminum alloy; and
forming, from a starting stock material, the final structural component by a one-step near-net-shape structural forming process using the forming tool with the MMC material placed in it, wherein the starting stock material comprises aluminum or an aluminum alloy and the forming includes inducing plastic deformation of the stock material, wherein the forming includes spin forming using a spinning mandrel and a series of rollers to shape the final structural component
wherein the one-step near-net-shape structural forming process comprises pressing the rollers to deform the stock material along a length of the spinning mandrel and bonding the MMC material in-situ to a surface of the final structural component.

16. The method of claim 15 , wherein:
the MMC material is a tape; and
the starting stock material is an aluminum-lithium alloy; and
the final structural component is a stiffenered aluminum-lithium alloy cylinder with the MMC material bonded to stiffeners formed integral with a wall of the of the stiffenered aluminum-lithium alloy cylinder.

17. The method of claim 1 , wherein the forming is performed at an elevated pressure and includes forming stiffeners integral with a wall of the final structural component when the spinning mandrel is rotated and the starting stock material is pressed against the spinning mandrel.

Assignees

• Nasa

Inventors

• Bird Richard Keith
• Alexa Joel A
• Messick Peter L
• Domack Marcia S
• Wagner John A

Classifications

• B21D49/00

  Sheathing or stiffening objects (by winding wire or tape thereon B65H54/00, B65H81/00; specially adapted for manufacturing conductors or cables H01B13/26) · CPC title

• B22D19/14

  the objects being filamentary or particulate in form (making alloys containing fibres or filaments by contacting the fibres or filaments with molten metal C22C47/08) · CPC title

• B21D37/01

  Selection of materials · CPC title

• B22D13/00

  Centrifugal casting; Casting by using centrifugal force · CPC title

• B21D22/16

  over shaping mandrels or formers · CPC title