Patent US4893743A successfully refreshed from Google Patents.
US4893743A
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Method to produce superplastically formed titanium aluminide components
Assignee: United States Department of the Air Force
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Filing: 1989-05-09
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Granted: 1990-01-16
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Expires: 2009-05-09
Abstract
Abstract Processes for producing titanium aluminide SPF/DB components, particularly structural panels, are provided. In one embodiment, the process comprises providing rapidly solidified titanium aluminide alloy sheetstock, providing a plurality of rapidly solidified titanium aluminide alloy ribbons or strips, forming the ribbons into waveform structures, assembling a plurality of these waveform structures to produce a honeycomb core, positioning this core between face sheets, and bonding the core to the face sheets. In another embodiment, the process comprises providing rapidly solidified titanium aluminide alloy sheetstock, superplastically forming at least one piece of sheetstock into a shaped piece having spaced apart, parallel bonding regions, positioning this shaped piece between two face sheets, and bonding the shaped piece to each face sheet. In yet another embodiment, the process comprises providing rapidly solidified titanium aluminide alloy sheetstock, applying a diffusion bond-inhibiting material in a desired pattern to at least one piece of sheetstock, assembling the sheetstock having the bond-inhibiting pattern thereon with at least one further piece of sheetstock, diffusion bonding this assembly, and superplastically forming the bonded assembly by introducing an inert gas into the region defined by the bond-inhibiting material.
Inventors
- 👤 Daniel Eylon
- 👤 Francis H. Froes
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-05 15:03
CPC Classifications
B; B23; B23K; B23K20/00; B21; B21D; B21D47/00
Claims Analysis
Total Claims: 18
Claim 1
Independent Claim
67 words
A method for producing a titanium aluminide honeycomb-core structural panel which comprises the steps of: (a) forming a plurality of rapidly solidified titanium aluminide strips into waveform structures; (b) assembling a plurality of said waveform structures to produce a honeycomb core; (c) positioning said core between two cover pieces of rapidly solidified titanium aluminide sheetstock; and (d) diffusion bonding said core to each of said cover pieces.
Claim 2
Independent Claim
67 words
A method for producing a titanium aluminide honeycomb-core structural panel which comprises the steps of: (a) forming a plurality of rapidly solidified titanium aluminide strips into waveform structures; (b) assembling a plurality of said waveform structures to produce a honeycomb core; (c) positioning said core between two cover pieces of rapidly solidified titanium aluminide sheetstock; and (d) diffusion bonding said core to each of said cover pieces.
Claim 3
Dependent Claim
41 words
The method of claim 1 wherein said sheetstock is fabricated from rapidly solidified foil by diffusion bonding a plurality of layers of foil under bonding conditions which permit retention of the uniform and fine grain microstructure of said rapidly solidified foil.
Claim 4
Dependent Claim
10 words
The method of claim 2 wherein said strips are sheetstock.
Claim 5
Dependent Claim
53 words
The method of claim 1 wherein said strips are relatively thick foil fabricated from relatively thin rapidly solidified foil by diffusion bonding a plurality of layers of said relatively thin rapidly solidified foil under bonding conditions which permit retention of the uniform and fine grain microstructure of said relatively thin rapidly solidified foil.
Claim 6
Dependent Claim
19 words
The method of claim 1 wherein said waveform structures are joined together during assembly to produce said honeycomb core.
Claim 7
Dependent Claim
15 words
The method of claim 5 wherein said waveform structures are joined together by diffusion bonding.
Claim 8
Dependent Claim
34 words
The method of claim 5 wherein said waveform structures are joined together by a fugitive thermoplastic binder material and wherein said fugitive binder is removed prior to bonding said core to said cover pieces.
Claim 9
Dependent Claim
47 words
The method of claim 1 wherein diffusion bonding is carried out at a temperature about 25° to 300° C. below the beta-transus temperature of said titanium aluminide at a pressure of about 10 to about 300 MPa for about 15 minutes to about 24 hours or more.
Claim 10
Independent Claim
96 words
A method for producing a titanium aluminide structural panel which comprises the steps of: (a) depositing a patterned coating of bond-inhibiting material onto at least one face surface of at least one sheet of rapidly solidified titanium aluminide sheetstock to provide a pattern-coated sheet; (b) assembling said pattern-coated sheet with at least one other sheet of rapidly solidified titanium aluminide sheetstock to provide a non-bonded assembly; (c) diffusion bonding said non-bonded assembly to provide a bonded assembly; and (d) introducing an inert gas into the region defined by said bond-inhibiting material to superplastically form said panel.
Claim 11
Independent Claim
96 words
A method for producing a titanium aluminide structural panel which comprises the steps of: (a) depositing a patterned coating of bond-inhibiting material onto at least one face surface of at least one sheet of rapidly solidified titanium aluminide sheetstock to provide a pattern-coated sheet; (b) assembling said pattern-coated sheet with at least one other sheet of rapidly solidified titanium aluminide sheetstock to provide a non-bonded assembly; (c) diffusion bonding said non-bonded assembly to provide a bonded assembly; and (d) introducing an inert gas into the region defined by said bond-inhibiting material to superplastically form said panel.
Claim 12
Dependent Claim
41 words
The method of claim 9 wherein said sheetstock is fabricated from rapidly solidified foil by diffusion bonding a plurality of layers of foil under bonding conditions which permit retention of the uniform and fine grain microstructure of said rapidly solidified foil.
Claim 13
Dependent Claim
50 words
The method of claim 9 wherein superplastic forming and diffusion bonding is carried out at a temperature about 25° to 300° C. below the bela-transus temperature of said titanium aluminide at a pressure of about 10 to about 300 MPa for about 15 minutes to about 24 hours or more.
Claim 14
Independent Claim
71 words
A method for producing a titanium aluminide structural panel which comprises the steps of: (a) superplastically forming at least one sheet of rapidly solidified titanium aluminide sheetstock into a shaped piece having a plurality of spaced apart, parallel bonding regions; (b) positioning said shaped piece between two sheets of rapidly solidified titanium aluminide sheetstock to provide a non-bonded assembly; and (c) diffusion bonding said non-bonded assembly to provide a bonded assembly.
Claim 15
Independent Claim
71 words
A method for producing a titanium aluminide structural panel which comprises the steps of: (a) superplastically forming at least one sheet of rapidly solidified titanium aluminide sheetstock into a shaped piece having a plurality of spaced apart, parallel bonding regions; (b) positioning said shaped piece between two sheets of rapidly solidified titanium aluminide sheetstock to provide a non-bonded assembly; and (c) diffusion bonding said non-bonded assembly to provide a bonded assembly.
Claim 16
Dependent Claim
41 words
The method of claim 12 wherein said sheetstock is fabricated from rapidly solidified foil by diffusion bonding a plurality of layers of foil under bonding conditions which permit retention of the uniform and fine grain microstructure of said rapidly solidified foil.
Claim 17
Dependent Claim
50 words
The method of claim 12 wherein superplastic forming and diffusion bonding is carried out at a temperature about 25° to 300° C. below the beta-transus temperature of said titanium aluminide at a pressure of about 10 to about 300 MPa for about 15 minutes to about 24 hours or more.
Claim 18
Dependent Claim
16 words
The method of claim 12 wherein said shaped piece comprises a plurality of spaced apart wells.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1993-01-15 | 1993-07-17 | 1994-01-16 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1997-01-15 | 1997-07-17 | 1998-01-16 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2001-01-15 | 2001-07-17 | 2002-01-16 | $7700.00 | Window Closed / Lapsed |