Patent US3713875A successfully refreshed from Google Patents.
US4480959A
Expired / Lapsed
US
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Device for damping vibrations of mobile turbine blades
Assignee: Safran Aircraft Engines SAS
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Filing: 1983-03-14
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Granted: 1984-11-06
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Expires: 2003-03-14
Abstract
Abstract A device for damping vibrations of mobile turbine blades, in which the roots of the blades are engaged in recesses distributed over the periphery of a rotor disk on which is anchored, under the rim of the disk, a leading edge flange consisting of sections and a trailing edge flange consisting of a single annular part against which the blade roots and the teeth of the disk rest. Between the root of a blade and the bottom of the recess of the disk is placed, behind the forward flange, a shim in the shape of a wedge which, under the action of centrifugal force, exerts on the blade a force that causes the blade to slide axially so that it contacts trailing edge retaining flange.
Inventors
- 👤 Serge P. L. Bourguignon
- 👤 Raymond R. Choque
- 👤 Lucien P. Pham
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 20:58
CPC Classifications
F; F16; F16F; F16F15/00; F01; F01D; F01D5/00; F01D5/12; F01D5/26; F01D5/30; F01D5/3007; F01D5/3015; Y; Y10; Y10S; Y10S416/00; Y10S416/50
Claims Analysis
Total Claims: 3
Claim 1
Independent Claim
242 words
A device for damping vibrations of at least first and second mobile turbine blades, in which the roots of the first and second blades are engaged in recesses distributed over the periphery of a rotor disk having a plurality of teeth, comprising: a first flange anchored under a first rim portion of said disk and which is operatively associated with a leading edge face of the disk and comprising sections that extend radially outward before the front faces of not greater than first and second adjacent blade roots; a second flange mounted under a second rim portion of said disk and which is operatively associated with a trailing edge face of said disk and comprising a single annular part, a portion of which extends radially outward a distance sufficient that the blade feet may contact it; and a shim member positioned between the root of the first blade and the bottom portion of one of said recesses in the disk, also being positioned behind the first flange, said shim member being in the shape of a wedge, which, under the action of centrifugal force, exerts on the first blade a force that causes the first blade to slide axially so as to exert a force on said second flange, wherein said second flange further comprises a first rib for contacting the root of said first blade and a second rib separated by a predetermined clearance from the trailing edge of the disk.
Claim 2
Independent Claim
242 words
A device for damping vibrations of at least first and second mobile turbine blades, in which the roots of the first and second blades are engaged in recesses distributed over the periphery of a rotor disk having a plurality of teeth, comprising: a first flange anchored under a first rim portion of said disk and which is operatively associated with a leading edge face of the disk and comprising sections that extend radially outward before the front faces of not greater than first and second adjacent blade roots; a second flange mounted under a second rim portion of said disk and which is operatively associated with a trailing edge face of said disk and comprising a single annular part, a portion of which extends radially outward a distance sufficient that the blade feet may contact it; and a shim member positioned between the root of the first blade and the bottom portion of one of said recesses in the disk, also being positioned behind the first flange, said shim member being in the shape of a wedge, which, under the action of centrifugal force, exerts on the first blade a force that causes the first blade to slide axially so as to exert a force on said second flange, wherein said second flange further comprises a first rib for contacting the root of said first blade and a second rib separated by a predetermined clearance from the trailing edge of the disk.
Claim 3
Dependent Claim
29 words
A device as set forth in claim 1, wherein the shim member further comprises a plate member extending between the first flange and the root of the first blade.
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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) | 1987-11-06 | 1988-05-07 | 1988-11-06 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1991-11-06 | 1992-05-07 | 1992-11-06 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1995-11-06 | 1996-05-07 | 1996-11-06 | $7700.00 | Window Closed / Lapsed |