Patent ID: 11938541
Assignee: THE BOEING COMPANY
Field: Materials, metallurgy (Chemistry)
Classification: CPC B | IPC B

Claim 9:
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.