Patent US4924581A successfully refreshed from Google Patents.
US4924581A
Expired / Lapsed
US
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Turbine air seal repair process
Assignee: Techniair Inc
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Filing: 1988-11-22
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Granted: 1990-05-15
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Expires: 2008-11-22
Abstract
Abstract A repair process for repairing damaged turbine air seals comprises completely removing the damaged air seals and forming a mechanical seat in the seal base. A replacement ring of the desired seal alloy is positioned in the seat and bonded to the base by a brazing process. The replacement ring is then machined to form reconstructed knife edge seals.
Inventors
- 👤 Karl S. Jakobsen
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 18:17
CPC Classifications
B; B23; B23P; B23P6/00; B23P6/002; B23P6/005; F; F01; F01D; F01D11/00; F01D11/08; F01D11/12; Y; Y10; Y10T; Y10T29/00; Y10T29/49; Y10T29/49316; Y10T29/49318; Y10T29/49718; Y10T29/49719; Y10T29/49721; Y10T29/49723; Y10T29/49725; Y10T29/49726; Y10T29/49728; Y10T29/4973; Y10T29/49732; Y10T29/49734; Y10T29/49737; Y10T29/49742
Claims Analysis
Total Claims: 13
Claim 1
Independent Claim
101 words
A repair process for repairing damaged turbine air seals which are formed from a seal assembly having at least one projecting seal member comprising: (a) completely removing at least one damaged seal member from said seal assembly to form a base; (b) machining said base to form a recess defining a mechanical seat; (c) providing a replacement member which is dimensioned to be closely received in said seat; (d) positioning said replacement member in said seat; (e) bonding said replacement member to said seal base by a brazing process; and (f) machining said replacement member to form a reconstructed seal member.
Claim 2
Dependent Claim
101 words
A repair process for repairing damaged turbine air seals which are formed from a seal assembly having at least one projecting seal member comprising: (a) completely removing at least one damaged seal member from said seal assembly to form a base; (b) machining said base to form a recess defining a mechanical seat; (c) providing a replacement member which is dimensioned to be closely received in said seat; (d) positioning said replacement member in said seat; (e) bonding said replacement member to said seal base by a brazing process; and (f) machining said replacement member to form a reconstructed seal member.
Claim 3
Dependent Claim
23 words
The repair process of claim 1 wherein step (a) comprises machining said assembly to completely remove a plurality of transversely spaced seal members.
Claim 4
Dependent Claim
29 words
The repair process of claim 2 wherein step (f) comprises forming a plurality of spaced reconstructed seal members having a transverse spacing generally equivalent to the removed seal members.
Claim 5
Dependent Claim
36 words
The repair process of claim 1 wherein step (b) comprises removing material from said seal base to form a recess having a width which is greater than the maximum transverse extent of the removed seal members.
Claim 6
Dependent Claim
20 words
The repair process of claim 1 wherein step (d) further comprises heating said seal base and cooling said replacement member.
Claim 7
Dependent Claim
170 words
A repair process for repairing damaged turbine air seals which are formed from an annular seal assembly having at least one radially projecting knife edge seal comprising: (a) completely removing at least one damaged knife edge seal from said assembly to form a base; (b) machining said base to form a recess defining a mechanical seat having a generally uniform width W and a depth d; (c) providing a replacement structure of the same material as the at least one removed knife edge seal and having a width which is approximately equal to width W and a thickness which is at least equal to the sum of depth d and the desired maximum radial projection of a knife edge seal from the base; (d) forcing the replacement structure into said seat so as to form a replacement ring; (e) bonding said replacement ring to said seal base by means of a high temperature brazing process; and (f) machining said replacement ring to form at least one reconstructed knife edge seal.
Claim 8
Dependent Claim
170 words
A repair process for repairing damaged turbine air seals which are formed from an annular seal assembly having at least one radially projecting knife edge seal comprising: (a) completely removing at least one damaged knife edge seal from said assembly to form a base; (b) machining said base to form a recess defining a mechanical seat having a generally uniform width W and a depth d; (c) providing a replacement structure of the same material as the at least one removed knife edge seal and having a width which is approximately equal to width W and a thickness which is at least equal to the sum of depth d and the desired maximum radial projection of a knife edge seal from the base; (d) forcing the replacement structure into said seat so as to form a replacement ring; (e) bonding said replacement ring to said seal base by means of a high temperature brazing process; and (f) machining said replacement ring to form at least one reconstructed knife edge seal.
Claim 9
Dependent Claim
24 words
The repair process of claim 6 wherein step (a) comprises machining said assembly to completely remove a plurality of transversely spaced knife edge seals.
Claim 10
Dependent Claim
31 words
The repair process of claim 7 wherein step (f) comprises forming a plurality of spaced reconstructed knife edge seals having a transverse spacing generally equivalent to the removed knife edge seals.
Claim 11
Dependent Claim
41 words
The repair process of claim 6 wherein step (b) further comprises removing material from said seal base to form a recess having a width which is greater than the maximum transverse extent of the at least one removed knife edge seal.
Claim 12
Dependent Claim
20 words
The repair process of claim 6 wherein step (d) further comprises heating said seal base and cooling said replacement structure.
Claim 13
Dependent Claim
20 words
The repair process of claim 10 wherein step (d) further comprises forcing said seal base into a true round condition.
References Cited (Backward Citations)
US4028788A
Cited
US4285108A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1993-05-14 | 1993-11-13 | 1994-05-15 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1997-05-14 | 1997-11-13 | 1998-05-15 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2001-05-14 | 2001-11-13 | 2002-05-15 | $7700.00 | Window Closed / Lapsed |