US4581300A
Expired / Lapsed
US
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Dual alloy turbine wheels
Assignee: Garrett Corp
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Filing: 1982-09-21
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Granted: 1986-04-08
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Expires: 2002-09-21
Abstract
Abstract A dual alloy turbine wheel manufacture of a cast integral blade ring pressure-sealed to a wrought alloy hub and thereafter bonded thereto by hot isostatic pressing.
Inventors
- 👤 George S. Hoppin, III
- 👤 George Curbishley
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-25 16:03
CPC Classifications
B; B23; B23P; B23P15/00; B23P15/006; B23K; B23K20/00; F; F01; F01D; F01D5/00; F01D5/30; F01D5/3061; B23K2101/00; B23K2101/001; F05; F05D; F05D2220/00; F05D2220/50; F05D2300/00; F05D2300/60; F05D2300/603; Y; Y10; Y10T; Y10T29/00; Y10T29/49; Y10T29/49316; Y10T29/4932; Y10T428/00; Y10T428/12; Y10T428/12014
Claims Analysis
Total Claims: 17
Claim 1
Independent Claim
178 words
A method for manufacturing a dual alloy turbine wheel having a superalloy blade ring of high creep rupture strength at temperatures up to about 1800 degrees F., and a superalloy hub of high tensile strength and highly resistant to low cycle fatique at tensile stress of at least 150,000 psi, to form a direct metallurgical bond between said hub and said ring, comprising the steps of: (a) preforming said blade ring and said hub with said ring ID shaped to receive the outer circumferential surface of said hub in near full surface area contact at the ring-hub surface interface; (b) assembling said hub in said ring with a deformable plate member of relatively thin-section temperature resistant material enclosing the ring-hub interface area; (c) bonding said plate member to said ring-hub assemblage to effect a vacuum seal between said ring, said hub and said plate member and (d) subjecting said sealing plate member and ring-hub assemblage to hot isostatic pressing at a hot isostatic pressing temperature and pressure to effect direct metallurgical bonding of said ring to said hub.
Claim 2
Independent Claim
178 words
A method for manufacturing a dual alloy turbine wheel having a superalloy blade ring of high creep rupture strength at temperatures up to about 1800 degrees F., and a superalloy hub of high tensile strength and highly resistant to low cycle fatique at tensile stress of at least 150,000 psi, to form a direct metallurgical bond between said hub and said ring, comprising the steps of: (a) preforming said blade ring and said hub with said ring ID shaped to receive the outer circumferential surface of said hub in near full surface area contact at the ring-hub surface interface; (b) assembling said hub in said ring with a deformable plate member of relatively thin-section temperature resistant material enclosing the ring-hub interface area; (c) bonding said plate member to said ring-hub assemblage to effect a vacuum seal between said ring, said hub and said plate member and (d) subjecting said sealing plate member and ring-hub assemblage to hot isostatic pressing at a hot isostatic pressing temperature and pressure to effect direct metallurgical bonding of said ring to said hub.
Claim 3
Dependent Claim
20 words
The method of claim 1 including the step of removing said plate member from said hot isostatic bonding ring-hub assemblage.
Claim 4
Dependent Claim
30 words
The method of claim 1 wherein said plate member is bonded to said ring by electron beam welding to effect said vacuum seal between said ring, hub and plate member.
Claim 5
Dependent Claim
31 words
The method of claim 1 wherein said plate member is bonded to said ring by diffusion brazing to effect said vacuum seal between said ring, said hub and said plate member.
Claim 6
Dependent Claim
73 words
The method of claim 1 wherein said ring-hub assemblage is preassembled prior to hot isostatic pressing with said plate member covering the exposed portion of said ring-hub interface, and said plate member is affixed to said assemblage by first electron beam welding said plate member to said ring, and thereafter a secondary seal of said interface is effected by applying a braze bead between said plate member and said ring by diffusion brazing.
Claim 7
Dependent Claim
22 words
The method of claim 1 wherein said hot isostatically pressed dual alloy turbine wheel is solution annealed, thermally stabilized, and thermally aged.
Claim 8
Dependent Claim
17 words
The method of claim 1 wherein said hub and ring alloys are nickel base gamma-prime strengthened alloys.
Claim 9
Dependent Claim
13 words
The method of claim 1 wherein said hub member is preformed by forging.
Claim 10
Dependent Claim
25 words
The method of claim 1 wherein said hub member is comprised of loose unconsolidated alloy powder which is consolidated during said hot isostatic pressing treatment.
Claim 11
Dependent Claim
34 words
The method of claim 1 wherein said hot isostatic pressing is conducted in an autoclave at a temperature in the range of 200° to 2300° F. at a pressure of at least 10,000 psi.
Claim 12
Dependent Claim
19 words
The method of claim 1 wherein said hub is sealed within said ring with an imperforate deformable plate member.
Claim 13
Dependent Claim
16 words
The dual alloy turbine wheel assemblage of claim 11 wherein said pressure transmitting membrane is imperforate.
Claim 14
Dependent Claim
43 words
The dual alloy turbine wheel of claim 1 wherein said ring is a cast nickel base superalloy containing a relative high proportion of gamma-prime forming elements and said hub is a wrought nickel base superalloy of a lower proportion of gamma-prime forming elements.
Claim 15
Dependent Claim
18 words
The method of claim 1 wherein said hub member is preformed by consolidation of loose unconsolidated prealloyed powder.
Claim 16
Dependent Claim
109 words
A vacuum sealed dual alloy turbine wheel assemblage having an integral blade ring of an alloy of high creep rupture strength at temperatures up to about 1800 degrees F. and a hub of an alloy of high tensile strength and which is highly resistant to low cycle fatigue at tensile stress of at least 150,000 psi, joined with an expendable temperature resistant membrane by bonding said membrane to said ring to vacuum seal said hub-ring interface, said membrane being functional to transmit pressure encountered during hot isostatic pressing to said sealed hub and ring to effect a direct metallurgical bond at said interface between said hub and said ring.
Claim 17
Dependent Claim
109 words
A vacuum sealed dual alloy turbine wheel assemblage having an integral blade ring of an alloy of high creep rupture strength at temperatures up to about 1800 degrees F. and a hub of an alloy of high tensile strength and which is highly resistant to low cycle fatigue at tensile stress of at least 150,000 psi, joined with an expendable temperature resistant membrane by bonding said membrane to said ring to vacuum seal said hub-ring interface, said membrane being functional to transmit pressure encountered during hot isostatic pressing to said sealed hub and ring to effect a direct metallurgical bond at said interface between said hub and said ring.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1989-04-07 | 1989-10-07 | 1990-04-08 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1993-04-07 | 1993-10-07 | 1994-04-08 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1997-04-07 | 1997-10-07 | 1998-04-08 | $7700.00 | Window Closed / Lapsed |