Patent US3713875A successfully refreshed from Google Patents.
← Back to Patent Explorer
US4480959A Expired / Lapsed US ⏱️ 0.0 years remaining

Device for damping vibrations of mobile turbine blades

Assignee: Safran Aircraft Engines SAS
•
Filing: 1983-03-14
•
Granted: 1984-11-06
•
Expires: 2003-03-14
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

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.

References Cited (Backward Citations)

US2836392A Cited
US3181835A Cited
US3455537A Cited
US3689177A Cited
US3768924A Cited
US3887298A Cited
FR2324873A1 Cited
US4021138A Cited
US4108571A Cited
FR2413542A1 Cited
US4192633A Cited

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

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag