IP Library Granted Patent US 10,094,013
Granted Patent B2
US 10,094,013 · App. 14/972,972 · Granted Oct 9, 2018

Method to prevent abnormal grain growth for beta annealed TI-6AL-4V forgings

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Quick Facts
Patent No.
US 10,094,013
App. No.
14/972,972
Granted
Oct 9, 2018
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 (28)

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

recrystallization annealing the titanium alloy, wherein recrystallization annealing comprises heating the titanium alloy to a temperature 30° F. to 200° F. below 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 after to 1200° 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.

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

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

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

5. The method of claim 1 , further comprising forging of the titanium alloy prior to the recrystallization annealing step.

6. The method of claim 1 , wherein the titanium alloy is Ti-6Al-4V.

7. The method of claim 1 , wherein the step of slow cooling the titanium alloy comprises furnace cooling the titanium alloy.

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 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, wherein the titanium alloy is Ti-6Al-4V, the method comprising the 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; and

beta annealing the titanium alloy following the furnace cooling step, wherein the beta annealing comprises heating the titanium alloy to a temperature in the range of 10° to 100° F. above beta transus of the titanium alloy for 15 minutes to 5 hours.

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

12. The method of claim 10 , wherein beta transus of the titanium alloy is a temperature between 1800° F. and 1850° F.

13. The method of claim 10 , further comprising steps of forging of the titanium alloy prior to the recrystallization annealing step.

14. The method of claim 10 , further comprising a step of heating then holding the titanium alloy at a stabilization temperature of between 1200° F. to 1450° F. following the step of furnace cooling and immediately preceding the step of beta annealing.

15. The method of claim 10 , 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.

16. The method of claim 10 , wherein the recrystallization annealing includes holding the titanium alloy at the temperature in the range of 30° F. to 200° F. below beta transus of the titanium alloy for a length of time in a range of 1 hour to 4 hours.

17. A method for heat-treating a titanium alloy, wherein the titanium alloy is Ti-6Al-4V, the method comprising the steps of:

forging of the titanium alloy such that localized, highly deformed grains are formed in the titanium alloy;

recrystallization annealing the titanium alloy by heating and holding the titanium alloy at a temperature in a range between 30° F. to 200° F. below beta transus of the titanium alloy for a length of time in a range of 1 to 4 hours following the forging step, then furnace cooling the titanium alloy to 1200° F. to 1500° F. at a rate of 50° F. to 500° F. per hour, wherein beta transus of the titanium alloy is a temperature between 1800° F. and 1850° F., wherein the recrystallization annealing results in the highly deformed grains forming fine and uniform transformed beta grains throughout the titanium alloy; and

beta annealing the titanium alloy following the furnace cooling, wherein the beta annealing comprises:

reheating then holding the titanium alloy at the temperature in the range between 30° F. to 200° F. below beta transus of the titanium alloy, and

heating then holding the titanium alloy at a temperature above beta transus of the titanium alloy for an amount of time between 15 minutes to 5 hours.

18. The method of claim 17 , 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.

19. The method of claim 17 , wherein the beta annealing further comprises holding the temperature in a range of 10° to 100° F. above the beta transus for 30 minutes per inch of thickness of the titanium alloy.

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 Dec 17, 2015
From: NASSERRAFI, RAHBAR; CLASPER, CRAIG M.; WALKER, MICHAEL A.; HICKS, GERALD E.
To: SPIRIT AEROSYSTEMS, INC.
Reel/Frame 037319/0685 →