Methods for manufacturing a wrought metallic article from a metallic-powder composition

Patent metadata

Field	Value
Publication number	US-11938541-B2
Application number	US-202117342690-A
Country	US
Kind code	B2
Filing date	Jun 9, 2021
Priority date	Dec 18, 2020
Publication date	Mar 26, 2024
Grant date	Mar 26, 2024

Abstract

A method for manufacturing a wrought metallic article from metallic-powder compositions comprises steps of (1) compacting the metallic-powder composition to yield a compact, having a surface, a cross-sectional area, and a relative density of less than 100 percent, (2) reducing the cross-sectional area of the compact via an initial forming pass of a rotary incremental forming process so that the compact has a decreased cross-sectional area, and (3) reducing the decreased cross-sectional area of the compact via a subsequent forming pass of the rotary incremental forming process by a greater percentage than that, by which the cross-sectional area of the compact was reduced during the initial forming pass.

First claim

What is claimed is:

1. A method for manufacturing a wrought metallic article from a metallic-powder composition, the method comprising steps of:
compacting the metallic-powder composition to yield a compact, having a surface, a cross-sectional area, and a relative density of less than 100 percent;
reducing the cross-sectional area of the compact via an initial forming pass of a rotary incremental forming process so that the compact has a decreased cross-sectional area, wherein the initial forming pass of the rotary incremental forming process reduces the cross-sectional area of the compact by at most 2 percent; and
reducing the decreased cross-sectional area of the compact via a subsequent forming pass of the rotary incremental forming process by a greater percentage than that, by which the cross-sectional area of the compact was reduced during the initial forming pass.

2. The method according to claim 1 , wherein an amount, by which the initial forming pass of the rotary incremental forming process reduces the cross-sectional area of the compact, is sufficient to close surface imperfections of the compact without damaging the compact.

3. The method according to claim 1 , wherein the step of compacting the metallic-powder composition comprises hydraulic pressing of the metallic-powder composition.

4. The method according to claim 1 , wherein the step of compacting the metallic-powder composition comprises cold isostatic pressing of the metallic-powder composition.

5. The method according to claim 1 , wherein the step of compacting the metallic-powder composition comprises hot isostatic pressing of the metallic-powder composition.

6. The method according to claim 1 , further comprising a step of sintering the compact prior to the step of reducing the cross-sectional area of the compact via the initial forming pass.

7. The method according to claim 1 , wherein the metallic-powder composition comprises titanium.

8. The method according to claim 1 , wherein the metallic-powder composition comprises Ti-6Al-4V.

9. The method according to claim 1 , wherein the metallic-powder composition comprises Ti-5Al-5Mo-5V-3Cr.

10. The method according to claim 1 , wherein the metallic-powder composition comprises at least one of aluminum; aluminum alloy; a metal-matrix composite, comprising aluminum; titanium; titanium alloy; a metal-matrix composite, comprising titanium; a superalloy; iron; iron alloy; a metal-matrix composite, comprising iron; nickel; nickel alloy; a metal-matrix composite, comprising nickel; cobalt; cobalt alloy; a metal-matrix composite, comprising cobalt; a refractory metal; a refractory metal alloy; a metal-matrix composite, comprising a refractory metal; copper; copper alloy; a metal-matrix composite, comprising copper; a precious metal; a precious-metal alloy; a metal-matrix composite, comprising a precious metal; zirconium; zirconium alloy; a metal-matrix composite, comprising zirconium; hafnium; hafnium alloy; a metal-matrix composite, comprising hafnium; intermetallics; a complex concentrated alloy; a metal-matrix composite, comprising a complex concentrated alloy; a high-entropy alloy; a metal-matrix composite, comprising a high-entropy alloy; a medium-entropy alloy; a metal-matrix composite, comprising a medium-entropy alloy; a multicomponent alloy; and a metal-matrix composite, comprising a multicomponent alloy.

11. The method according to claim 1 , further comprising blending a first metallic-powder component, having a first composition, with a second metallic-powder component, having a second composition, to yield the metallic-powder composition, wherein the first composition is different from the second composition.

12. The method according to claim 1 , wherein the metallic-powder composition comprises non-spherical particles.

13. The method according to claim 1 , wherein the metallic-powder composition has a particle-size distribution such that:
at least 90 percent of the metallic-powder composition is composed of particles, having a maximum dimension that is less than 170 μm,
at least 50 percent of the metallic-powder composition is composed of particles, having a maximum dimension that is less than 100 μm, and
at least 10 percent of the metallic-powder composition is composed of particles, having a maximum dimension that is less than 40 μm.

14. The method according to claim 1 , wherein:
the rotary incremental forming process is performed at a rotary-incremental-forming-process temperature (in degrees Kelvin), and
the rotary-incremental-forming-process temperature is at most 95 percent of a melting temperature (in degrees Kelvin) of the metallic-powder composition.

15. The method according to claim 1 , further comprising a step of annealing the compact after the step of reducing the decreased cross-sectional area of the compact via the subsequent forming pass of the rotary incremental forming process.

16. The method according to claim 1 , further comprising steps of:
during at least one of the initial forming pass or the subsequent forming pass, measuring a temperature of the compact along a predetermined portion of the surface of the compact using a beam of electromagnetic radiation;
determining a temperature differential between the temperature of the compact along the predetermined portion of the surface of the compact and a predefined target temperature; and
controlling, based on the temperature differential, at least one of a feed speed of the rotary incremental forming process or a rotational speed of the rotary incremental forming process during at least the one of the initial forming pass or the subsequent forming pass.

17. The method according to claim 16 , wherein the step of measuring the temperature of the compact along the predetermined portion of the surface of the compact using a beam of electromagnetic radiation, the step of determining the temperature differential between the temperature of the compact along the predetermined portion of the surface of the compact and the predefined target temperature, and the step of controlling, based on the temperature differential, at least one of the feed speed of the rotary incremental forming process or the rotational speed of the rotary incremental forming process during at least the one of the initial forming pass or the subsequent forming pass are performed in real time.

18. The method according to claim 1 , further comprising steps of:
during at least one of the initial forming pass or the subsequent forming pass, measuring a temperature of the compact along a predetermined portion of the surface of the compact using a beam of electromagnetic radiation;
during at least the one of the initial forming pass or the subsequent forming pass, measuring a temperature of the compact along a second predetermined portion of the surface of the compact using a second beam of electromagnetic radiation;
determining a temperature differential between the temperature of the compact along the predetermined portion of the surface of the compact and the temperature of the compact along the second predetermined portion of the surface of the compact; and
controlling, based on the temperature differential, at least one of a feed speed of the rotary incremental forming process or a rotational speed of the rotary incremental forming process during at least the one of the initial forming pass or the subsequent forming pass,
wherein the predetermined portion of the surface of the compact is at a different location on the surface than the second predetermined portion.

19. The me

Assignees

• Boeing Co

Inventors

• Mann Austin E
• Yousefiani Ali
• Pecina Joe

Classifications

• B22F3/17 Primary

  by forging · CPC title

• B22F3/12 Primary

  Both compacting and sintering (by forging B22F3/17) · CPC title

• B22F1/052

  characterised by a mixture of particles of different sizes or by the particle size distribution · CPC title

• B22F1/06

  Metallic powder characterised by the shape of the particles (nanosized particles B22F1/054) · CPC title

• B22F3/003

  Apparatus, e.g. furnaces (in general F27B) · CPC title