US4415375A
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Transient titanium alloys
Assignee: McDonnell Douglas Corp
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Filing: 1982-06-10
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Granted: 1983-11-15
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Expires: 2002-06-10
Abstract
Abstract Transient titanium alloys having the composition A-XH, where A is titanium or a titanium alloy, such as, Ti-8Al-1Mo-1V, Ti-5Al-2.5Sn, Ti-6Al-4V, or Ti-6Al-2Sn-4Zr-2Mo; where H represents hydrogen and where X is a weight percent value between about 0.01 and 0.5%. The alloys may be produced by heating the base titanium or titanium alloy under pressure in a non-flammable atmosphere containing hydrogen. The alloys containing hydrogen may be formed by superplastic forming techniques. After forming, the original titanium or titanium alloy can be restored by heating the formed part or structure, under vacuum, driving out the hydrogen from the alloy. Parts and structures formed from the transient alloy, and restored, retain the strength and structural integrity of the base alloy.
Inventors
- 👤 Richard J. Lederich
- 👤 Shankar M. Sastry
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-24 13:57
CPC Classifications
B; B21; B21D; B21D26/00; B21D26/02; B21D26/053; B21D26/055; C; C22; C22F; C22F1/00; C22F1/02; C22F1/16; C22F1/18; C22F1/183
Claims Analysis
Total Claims: 24
Claim 1
Independent Claim
51 words
The method of superplastically forming of titanium and titanium alloys comprising treating a stock piece of titanium or titanium alloy in a hydrogen containing atmosphere causing absorption of hydrogen into the matrix of the stock part in an amount effective to improve forming, and forming the treated stock in a die.
Claim 2
Independent Claim
51 words
The method of superplastically forming of titanium and titanium alloys comprising treating a stock piece of titanium or titanium alloy in a hydrogen containing atmosphere causing absorption of hydrogen into the matrix of the stock part in an amount effective to improve forming, and forming the treated stock in a die.
Claim 3
Dependent Claim
17 words
The method of claim 1 wherein the hydrogen is present between about 0.01 to 0.5 weight percent.
Claim 4
Dependent Claim
43 words
The alloy of claim 1 wherein the method has the formula A--XH where A is selected from the group consisting of titanium and titanium alloys, where H is hydrogen and where X is a value of between about 0.01 to 0.5 weight percent.
Claim 5
Dependent Claim
22 words
The method of claim 3 wherein the titanium alloy is selected from the group consisting of Ti-8Al-1Mo-1V, Ti-5Al-2.5Sn, Ti-6Al-V and Ti-6Al-2Sn-4Zr-2Mo alloys.
Claim 6
Dependent Claim
23 words
The method of claim 3 wherein the titanium alloy is selected from the group consisting of high temperature and near alpha titanium alloys.
Claim 7
Dependent Claim
21 words
The method of claim 1 wherein the treated stock is in sheet form of between about 0.040 and 3/16 inches thickness.
Claim 8
Dependent Claim
13 words
The method of claim 1 including removing the hydrogen from the formed stock.
Claim 9
Dependent Claim
22 words
The method of claim 7 wherein the formed stock is heated in at least a partial vacuum to remove the hydrogen therefrom.
Claim 10
Dependent Claim
19 words
The method of claim 9 wherein the formed stock is heated at a temperature of between about 600°-650° C.
Claim 11
Dependent Claim
20 words
The method of claim 1 wherein the stock is treated under elevated temperature and pressure in the hydrogen containing atmosphere.
Claim 12
Dependent Claim
28 words
The method of claim 10 wherein the stock is treated at a temperature of between about 600°-760° C. and at a pressure of at least about 50-300 psi.
Claim 13
Dependent Claim
19 words
The method of claim 10 wherein the stock is treated in an atmosphere containing up to about 5% hydrogen.
Claim 14
Independent Claim
143 words
The method of superplastically forming titanium and titanium alloy sheets to form complex parts comprising introducing a sheet of titanium or titanium alloy into a die, introducing a hydrogen containing atmosphere into the die at an elevated temperature and an elevated pressure, adsorbing hydrogen into the titanium or titanium alloy sheet to form a transient alloy containing hydrogen, the hydrogen being absorbed into the alloy matrix in an amount effective to improve superplastic forming of the sheet, releasing the pressure on one side of the titanium or titanium alloy sheet and increasing the pressure on the remaining side of the sheet causing the sheet to flow into and conform to the shape of the die and restoring the titanium or titanium alloy sheet to its original composition under temperature conditions effective to maintain the ductility of the original titanium or titanium alloy sheet.
Claim 15
Independent Claim
143 words
The method of superplastically forming titanium and titanium alloy sheets to form complex parts comprising introducing a sheet of titanium or titanium alloy into a die, introducing a hydrogen containing atmosphere into the die at an elevated temperature and an elevated pressure, adsorbing hydrogen into the titanium or titanium alloy sheet to form a transient alloy containing hydrogen, the hydrogen being absorbed into the alloy matrix in an amount effective to improve superplastic forming of the sheet, releasing the pressure on one side of the titanium or titanium alloy sheet and increasing the pressure on the remaining side of the sheet causing the sheet to flow into and conform to the shape of the die and restoring the titanium or titanium alloy sheet to its original composition under temperature conditions effective to maintain the ductility of the original titanium or titanium alloy sheet.
Claim 16
Dependent Claim
23 words
The method of claim 13 wherein hydrogen is absorbed into the sheet at a level of between about 0.01 and 0.5 weight percent.
Claim 17
Dependent Claim
28 words
The method of claim 13 wherein the transient hydrogen containing alloy formed contains hydrogen in an amount less than that capable of producing a single beta phase alloy.
Claim 18
Dependent Claim
23 words
The method of claim 13 wherein the grain size of the titanium or titanium alloy formed part is maintained below about 10 microns.
Claim 19
Dependent Claim
29 words
The method of claim 13 wherein the titanium or titanium alloy sheet is restored to its original composition at a temperature below that at which substantial grain coarsening occurs.
Claim 20
Dependent Claim
70 words
A titanium or titanium alloy formed part, the part being superplastically formed by the method of claim 15, the formed part being of a sheet stock between about 0.040 and 3/16 inch thickness, the as formed part substantially retaining the ductility and strength of the original titanium or titanium alloy sheet stock used in forming the part, the as formed part having a grain size of below about 10 microns.
Claim 21
Independent Claim
229 words
The method of superplastically forming titanium and titanium alloy sheets to form complex parts comprising introducing a sheet of titanium or titanium alloy into a die, the sheet being between about 0.040 and 3/16 inches in thickness, introducing a hydrogen containing atmosphere into the die at an elevated temperature of between about 600°-760° C. and an elevated pressure of at least about 50-300 psi, absorbing hydrogen into the titanium or titanium alloy sheet to form a transient alloy containing hydrogen, the hydrogen being absorbed into the alloy matrix in an amount between about 0.01 and 0.5 weight percent less than an amount producing a single phase alloy and being effective to improve superplastic forming of the sheet, releasing the pressure on one side of the titanium or titanium alloy sheet and increasing the pressure on the remaining side of the sheet causing the sheet to flow into and conform to the shape of the die and restoring the titanium or titanium alloy sheet to its original composition while maintaining the strength and ductility of the original titanium or titanium alloy sheet, including heating the formed sheet at a temperature of between about 600°-650° C., the method being effective to increase the speed of superplastic forming of the titaium or titanium alloy sheet and reduce the wear on the die in which the titanium or titanium alloy sheet is formed.
Claim 22
Independent Claim
229 words
The method of superplastically forming titanium and titanium alloy sheets to form complex parts comprising introducing a sheet of titanium or titanium alloy into a die, the sheet being between about 0.040 and 3/16 inches in thickness, introducing a hydrogen containing atmosphere into the die at an elevated temperature of between about 600°-760° C. and an elevated pressure of at least about 50-300 psi, absorbing hydrogen into the titanium or titanium alloy sheet to form a transient alloy containing hydrogen, the hydrogen being absorbed into the alloy matrix in an amount between about 0.01 and 0.5 weight percent less than an amount producing a single phase alloy and being effective to improve superplastic forming of the sheet, releasing the pressure on one side of the titanium or titanium alloy sheet and increasing the pressure on the remaining side of the sheet causing the sheet to flow into and conform to the shape of the die and restoring the titanium or titanium alloy sheet to its original composition while maintaining the strength and ductility of the original titanium or titanium alloy sheet, including heating the formed sheet at a temperature of between about 600°-650° C., the method being effective to increase the speed of superplastic forming of the titaium or titanium alloy sheet and reduce the wear on the die in which the titanium or titanium alloy sheet is formed.
Claim 23
Dependent Claim
23 words
The method of claim 19 wherein the grain size of the titanium or titanium alloy formed sheet is maintained below about 10 microns.
Claim 24
Dependent Claim
40 words
The method of claim 19 wherein the titanium or titanium alloy is treated in an atmosphere containing up to about 5% hydrogen and wherein the formed sheet is heated in at least a partial vacuum to remove the hydrogen therefrom.
References Cited (Backward Citations)
US2892742A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1986-11-14 | 1987-05-16 | 1987-11-15 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1990-11-14 | 1991-05-16 | 1991-11-15 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1994-11-14 | 1995-05-16 | 1995-11-15 | $7700.00 | Window Closed / Lapsed |