IP Library Granted Patent US 10,822,682
Granted Patent B2
US 10,822,682 · App. 16/151,512 · Granted Nov 3, 2020

Method to prevent abnormal grain growth for beta annealed Ti—6AL—4V forgings

Inventors: Rahbar Nasserrafi (Andover, KS); Gerald E. Hicks (Wichita, KS); Michael A. Walker (Wichita, KS); Craig M. Clasper (Derby, KS)
Assignee: Spirit AeroSystems, Inc.
C22F1/183C22C14/00C22F1/02
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Quick Facts
Patent No.
US 10,822,682
App. No.
16/151,512
Granted
Nov 3, 2020
Kind
B2
Abstract

A method for heat-treating a titanium alloy, such as Ti-6Al-4V. The method may occur after or include a step of forging the titanium alloy such that localized, highly deformed grains are formed in the titanium alloy. Then the method may include steps of recrystallization annealing the titanium alloy by heating the titanium alloy to a temperature in a range between 30° F. to 200° F. below beta transus of the titanium alloy for 1 hour to 6 hours and then furnace cooling of the titanium alloy to 1200° F. to 1500° F. at a rate of 50° F. to 500° F. per hour. Following the recrystallization annealing, the method may include beta annealing the titanium alloy. These steps may be performed in a single heat treating cycle.

Claims (25)

1. A method for heat-treating a titanium alloy, the method comprising the steps of:

recrystallization annealing the titanium alloy, wherein recrystallization annealing includes heating the titanium alloy to a temperature below a beta transus of the titanium alloy for a length of time followed by slow cooling the titanium alloy; and

beta annealing the titanium alloy following completion of the recrystallization annealing steps by heating the titanium alloy to a temperature in a range of 10° to 100° F. above the beta transus of the titanium alloy.

2. The method of claim 1 , wherein the beta transus of the titanium alloy is a temperature between 1800° F. and 1850° F.

3. The method of claim 1 , wherein the temperature to which the titanium alloy is heated during recrystallization annealing is 30° F. to 200° F. below the beta transus of the titanium alloy.

4. The method of claim 1 , wherein the length of time for which the temperature below the beta transus of the titanium alloy is maintained during recrystallization annealing is in a range of 1 hour to 6 hours.

5. The method of claim 1 , wherein following heating the titanium alloy to the temperature below the beta transus of the titanium alloy for the length of time during recrystallization annealing, the titanium alloy is cooled to 1200° F. to 1500° F. at a rate of 50° F. to 500° F. per hour.

6. The method of claim 1 , wherein the beta annealing includes holding the temperature above the beta transus for 30 minutes per inch of thickness of the titanium alloy.

7. The method of claim 1 , wherein the beta annealing further includes holding the temperature in the range of 10° to 100° F. above the beta transus for 15 minutes to 5 hours.

8. The method of claim 1 , further comprising a step of gradually heating then holding the titanium alloy at a temperature 30° F. to 200° F. below the beta transus of the titanium alloy following the slow cooling of the recrystallization annealing step and immediately preceding the step of beta annealing.

9. The method of claim 8 , further comprising the steps of cooling the titanium alloy to a stabilization temperature between 1200° F. to 1450° F. for one or more hours following the beta annealing step and then cooling the titanium alloy to room temperature.

10. A method for heat-treating a titanium alloy, the method comprising the steps of:

recrystallization annealing the titanium alloy, wherein recrystallization annealing includes heating the titanium alloy to a temperature 30° F. to 200° F. below a beta transus of the titanium alloy for a length of time in a range of 1 hour to 6 hours followed by slow cooling the titanium alloy to 1000° F. to 1500° F. at a rate of 50° F. to 500° F. per hour; and

beta annealing the titanium alloy following completion of the recrystallization annealing steps, including heating the titanium alloy to a temperature in a range of 10° to 100° F. above the beta transus of the titanium alloy.

11. The method of claim 10 , wherein the beta annealing includes holding the temperature above the beta transus for 30 minutes per inch of thickness of the titanium alloy.

12. The method of claim 11 , wherein the beta annealing further includes holding the temperature in the range of 10° to 100° F. above the beta transus for 15 minutes to 5 hours.

13. The method of claim 10 , further comprising a step of gradually heating then holding the titanium alloy at a temperature 30° F. to 200° F. below the beta transus of the titanium alloy following the slow cooling of the recrystallization annealing step and immediately preceding the step of beta annealing.

14. The method of claim 13 , further comprising the steps of cooling the titanium alloy to a stabilization temperature between 1200° F. to 1450° F. for one or more hours following the beta annealing step and then cooling the titanium alloy to room temperature.

15. A method for heat-treating a titanium alloy, the method comprising the steps of:

recrystallization annealing the titanium alloy, wherein recrystallization annealing includes heating the titanium alloy to a temperature 30° F. to 200° F. below the beta transus of the titanium alloy for a length of time in a range of 1 hour to 6 hours followed by slow cooling the titanium alloy to 1000° F. to 1500° F. at a rate of 50° F. to 500° F. per hour; and

beta annealing the titanium alloy following completion of the recrystallization annealing steps, including heating the titanium alloy to a temperature above the beta transus of the titanium alloy and holding the temperature above the beta transus for at least 15 minutes per inch of thickness of the titanium alloy.

16. The method of claim 15 , wherein the beta transus of the titanium alloy is a temperature between 1800° F. and 1850° F.

17. The method of claim 15 , wherein the beta annealing further includes holding the temperature above the beta transus for 30 minutes to 5 hours.

18. The method of claim 15 , further comprising a step of gradually heating then holding the titanium alloy at a temperature 30° F. to 200° F. below the beta transus of the titanium alloy following the slow cooling of the recrystallization annealing step and immediately preceding the step of beta annealing.

19. The method of claim 18 , further comprising the steps of cooling the titanium alloy to a stabilization temperature between 1200° F. to 1450° F. for one or more hours following the beta annealing step and then cooling the titanium alloy to room temperature.

Assignments (15)
RELEASE OF SECURITY INTEREST Recorded Dec 11, 2025
From: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 073932/0669 →
RELEASE OF SECURITY INTEREST Recorded Dec 10, 2025
From: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 073900/0356 →
RELEASE OF SECURITY INTEREST Recorded Dec 9, 2025
From: MORGAN STANLEY SENIOR FUNDING, INC., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 073916/0346 →
SECURITY AGREEMENT Recorded Jul 8, 2024
From: SPIRIT AEROSYSTEMS, INC.
To: MORGAN STANLEY SENIOR FUNDING, INC.
Reel/Frame 068217/0456 →
RELEASE OF SECURITY INTEREST Recorded Dec 4, 2023
From: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
To: SPIRIT AEROSYSTEMS, INC.; SPIRIT AEROSYSTEMS HOLDINGS, INC.; SPIRIT AEROSYSTEMS NORTH CAROLINA, INC.
Reel/Frame 065772/0456 →
SECURITY AGREEMENT (SECOND LIEN NOTES) Recorded Nov 21, 2023
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS COLLATERAL AGENT
Reel/Frame 065659/0585 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Nov 23, 2022
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 061993/0847 →
RELEASE OF SECURITY INTEREST Recorded Nov 23, 2022
From: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A., AS COLLATERAL AGENT
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 061995/0281 →
RELEASE OF SECURITY INTEREST Recorded Oct 28, 2020
From: BANK OF AMERICA, N.A.
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 054230/0578 →
SECURITY INTEREST Recorded Oct 5, 2020
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 053993/0569 →
SECURITY INTEREST Recorded Oct 5, 2020
From: SPIRIT AEROSYSTEMS, INC.
To: BANK OF AMERICA, N.A.
Reel/Frame 053993/0505 →
SECURITY INTEREST Recorded Oct 5, 2020
From: SPIRIT AEROSYSTEMS, INC.
To: BANK OF AMERICA, N.A.
Reel/Frame 053983/0350 →
SECURITY INTEREST Recorded Apr 17, 2020
From: SPIRIT AEROSYSTEMS, INC.
To: THE BANK OF NEW YORK MELLON TRUST COMPANY, N.A.
Reel/Frame 052433/0843 →
NOTICE OF GRANT OF SECURITY INTEREST IN PATENTS Recorded Feb 24, 2020
From: SPIRIT AEROSYSTEMS, INC.
To: BANK OF AMERICA, N.A., AS COLLATERAL AGENT
Reel/Frame 052004/0929 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 4, 2018
From: NASSERRAFI, RAHBAR; WALKER, MICHAEL A; CLASPER, CRAIG M; HICKS, GERALD E
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 047066/0230 →
Continuity (3)
Continuation 14972972 · Dec 17, 2015
Provisional Application 62096079 · Dec 23, 2014
Related Publication 20190032184A1 · Jan 31, 2019