IP Library Granted Patent US 7,883,590
Granted Patent B1
US 7,883,590 · App. 12/939,345 · Granted Feb 8, 2011

Heat treatable L1

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Quick Facts
Patent No.
US 7,883,590
App. No.
12/939,345
Granted
Feb 8, 2011
Kind
B1
Abstract

A method of forming high temperature heat treatable aluminum alloys that can be used at temperatures from about −420° F. (−251° C.) up to about 650° F. (343° C.) are described. The alloys are strengthened by dispersion of particles based on the L1 2 intermetallic compound Al 3 X. These alloys comprise aluminum, copper, magnesium, at least one of scandium, erbium, thulium, ytterbium, and lutetium; and at least one of gadolinium, yttrium, zirconium, titanium, hafnium, and niobium. Lithium is an optional alloying element.

Claims (57)

1. A method of forming a heat treatable aluminum alloy, the method comprising:

(a) forming a melt consisting of:

about 1.0 to about 8.0 weight percent copper;

about 0.2 to about 4.0 weight percent magnesium;

about 0.5 to about 3.0 weight percent lithium;

at least one first element selected from the group consisting of about 0.1 to about 0.5 weight percent scandium, about 0.1 to about 6.0 weight percent erbium, about 0.1 to about 10.0 weight percent thulium, about 0.1 to about 15.0 weight percent ytterbium, and about 0.1 to about 12.0 weight percent lutetium;

at least one second element selected from the group consisting of about 0.1 to about 4.0 weight percent gadolinium, about 0.1 to about 4.0 weight percent yttrium, about 0.05 to about 1.0 weight percent zirconium, about 0.05 to about 2.0 weight percent titanium, about 0.05 to about 2.0 weight percent hafnium, and about 0.05 to about 1.0 weight percent niobium;

and the balance substantially aluminum;

(b) solidifying the melt to form a solid body; and

(c) heat treating the solid body.

2. The method of claim 1 , further comprising:

refining the structure of the solid body by deformation processing comprising at least one of: extrusion, forging and rolling.

3. The method of claim 1 , wherein solidifying comprises a casting process.

4. The method of claim 1 , wherein solidifying comprises a rapid solidification process in which the cooling rate is greater than about 10 3 ° C./second and comprising at least one of: powder processing, atomization, melt spinning, splat quenching, spray deposition, cold spray, plasma spray, laser melting, laser deposition, ball milling, and cryomilling.

5. The method of claim 1 , wherein the heat treating comprises:

solution heat treatment at about 800° F. (426° C.) to about 1100° F. (593° C.) for about thirty minutes to four hours;

quenching; and

aging at about 200° F. (93° C.) to about 600° F. (316° C.) for about two to forty-eight hours.

6. A method of forming a heat treatable aluminum alloy, the method comprising:

(a) forming a melt consisting of:

about 1.0 to about 8.0 weight percent copper;

about 0.2 to about 4.0 weight percent magnesium;

about 0.5 to about 3.0 weight percent lithium;

at least one first element selected from the group consisting of about 0.1 to about 0.5 weight percent scandium, about 0.1 to about 6.0 weight percent erbium, about 0.1 to about 10.0 weight percent thulium, about 0.1 to about 15.0 weight percent ytterbium, and about 0.1 to about 12.0 weight percent lutetium;

at least one second element selected from the group consisting of about 0.1 to about 4.0 weight percent gadolinium, about 0.1 to about 4.0 weight percent yttrium, about 0.05 to about 1.0 weight percent zirconium, about 0.05 to about 2.0 weight percent titanium, about 0.05 to about 2.0 weight percent hafnium, and about 0.05 to about 1.0 weight percent niobium;

consisting of no more than about 0.1 weight percent iron, about 0.1 weight percent chromium, about 0.1 weight percent manganese, about 0.1 weight percent vanadium, about 0.1 weight percent cobalt, and about 0.1 weight percent nickel;

no more than about 1.0 weight percent total other additional elements not listed therein including impurities;

and the balance substantially aluminum;

(b) solidifying the melt to form a solid body; and

(c) heat treating the solid body.

7. The method of claim 6 , further comprising:

refining the structure of the solid body by deformation processing comprising at least one of: extrusion, forging and rolling.

8. The method of claim 6 , wherein solidifying comprises a casting process.

9. The method of claim 6 , wherein solidifying comprises a rapid solidification process in which the cooling rate is greater than about 10 3 ° C./second and comprising at least one of: powder processing, atomization, melt spinning, splat quenching, spray deposition, cold spray, plasma spray, laser melting, laser deposition, ball milling, and cryomilling.

10. The method of claim 6 , wherein the heat treating comprises:

solution heat treatment at about 800° F. (426° C.) to about 1100° F. (593° C.) for about thirty minutes to four hours;

quenching; and

aging at about 200° F. (93° C.) to about 600° F. (316° C.) for about two to forty-eight hours.

11. A method of forming a heat treatable aluminum alloy, the method comprising:

(a) forming a melt consisting of:

about 1.0 to about 8.0 weight percent copper;

about 0.2 to about 4.0 weight percent magnesium;

about 0.5 to about 3.0 weight percent lithium;

at least one first element selected from the group consisting of about 0.1 to about 0.5 weight percent scandium, about 0.1 to about 6.0 weight percent erbium, about 0.1 to about 10.0 weight percent thulium, about 0.1 to about 15.0 weight percent ytterbium, and about 0.1 to about 12.0 weight percent lutetium;

at least one second element selected from the group consisting of about 0.1 to about 4.0 weight percent gadolinium, about 0.1 to about 4.0 weight percent yttrium, about 0.05 to about 1.0 weight percent zirconium, about 0.05 to about 2.0 weight percent titanium, about 0.05 to about 2.0 weight percent hafnium, and about 0.05 to about 1.0 weight percent niobium;

no more than about 1.0 weight percent total other additional elements not listed therein including impurities;

and the balance substantially aluminum;

(b) solidifying the melt to form a solid body; and

(c) heat treating the solid body.

12. The method of claim 11 , further comprising:

refining the structure of the solid body by deformation processing comprising at least one of: extrusion, forging and rolling.

13. The method of claim 11 , wherein solidifying comprises a casting process.

14. The method of claim 11 , wherein solidifying comprises a rapid solidification process in which the cooling rate is greater than about 10 3 ° C./second and comprising at least one of: powder processing, atomization, melt spinning, splat quenching, spray deposition, cold spray, plasma spray, laser melting, laser deposition, ball milling, and cryomilling.

15. The method of claim 11 wherein the heat treating comprises:

solution heat treatment at about 800° F. (426° C.) to about 1100° F. (593° C.) for about thirty minutes to four hours;

quenching; and

aging at about 200° F. (93° C.) to about 600° F. (316° C.) for about two to forty-eight hours.

Assignments (7)
TERMINATION AND RELEASE OF SECURITY INTEREST IN PATENTS Recorded Jul 28, 2023
From: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
To: AEROJET ROCKETDYNE, INC.
Reel/Frame 064424/0109 →
CHANGE OF NAME Recorded Jul 27, 2023
From: RAYTHEON TECHNOLOGIES CORPORATION
To: RTX CORPORATION
Reel/Frame 064714/0001 →
CORRECTIVE ASSIGNMENT TO CORRECT THE AND REMOVE PATENT APPLICATION NUMBER 11886281 AND ADD PATENT APPLICATION NUMBER 14846874. TO CORRECT THE RECEIVING PARTY ADDRESS PREVIOUSLY RECORDED AT REEL: 054062 FRAME: 0001. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF ADDRESS. Recorded Mar 4, 2021
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 055659/0001 →
CHANGE OF NAME Recorded Sep 4, 2020
From: UNITED TECHNOLOGIES CORPORATION
To: RAYTHEON TECHNOLOGIES CORPORATION
Reel/Frame 054062/0001 →
LICENSE Recorded Aug 5, 2016
From: UNITED TECHNOLOGIES CORPORATION
To: AEROJET ROCKETDYNE, INC. (F/K/A AEROJET-GENERAL CORPORATION, SUCCESSOR OF RPW ACQUISITION LLC)
Reel/Frame 039595/0315 →
RELEASE OF SECURITY INTEREST Recorded Aug 5, 2016
From: U.S. BANK NATIONAL ASSOCIATION
To: AEROJET ROCKETDYNE OF DE, INC. (F/K/A PRATT & WHITNEY ROCKETDYNE, INC.)
Reel/Frame 039597/0890 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Jun 17, 2016
From: AEROJET ROCKETDYNE, INC., SUCCESSOR-IN-INTEREST TO RPW ACQUISITION LLC
To: BANK OF AMERICA, N.A., AS ADMINISTRATIVE AGENT
Reel/Frame 039197/0125 →