Patent US4189282A successfully refreshed from Google Patents.
US4189282A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Device to secure vanes to a rotor
Assignee: Safran Aircraft Engines SAS
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Filing: 1978-06-05
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Granted: 1980-02-19
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Expires: 1998-06-05
Abstract
Abstract A device to secure and insure the tightness of vanes of a turbine is an alar plate which carries on the side toward its external edge a plurality of studs and toward its internal edge a plurality of hangers. The disk of the rotor has on its lower edge a series of teeth or indentations, the top of the teeth having a configuration to cooperate with the inner surface of the hangers. The vanes have on their rims a plurality of grooves. Two adjacent vanes form a groove into which the studs enter when the hangers cooperate with the teeth. The studs are borne by tongues cut radially into the annular plate.
Inventors
- 👤 Josette Benoist
- 👤 Pierre A. Glowacki
- 👤 Gerard M. F. Mandet
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-05 05:27
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/30; F01D5/3007; F01D5/3015
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
208 words
In a device for securing vanes to a turbine rotor wherein said rotor is a disk having a rim with a plurality of axial grooves on its outer periphery, vanes having roots extending slidably into said grooves and said device comprising at least one annular retaining check plate coaxial with said disk, abutting the ends of said roots, and means for securing said check plate in position, the improvement comprising: said securing means being in the form of radially inwardly extending projections on the radially inner edge of the rim, and generally hook-shaped hangers formed on the radially inner edge of the check plate and engaging said projections to prevent axial movement of said check plate away from said disk, said projections being spaced apart to define indentations for receiving said hangers, said hangers being engageable with and disengageable from said projections by rotating said check plate relative to said disk; elastic tongues defined by cuts extending radially inwardly from the radially outer edge of said check plate; axially extending studs at the outer ends of said tongues, extending toward said disk; and recesses in the adjacent ends of said vanes, said studs extending into said recesses to prevent rotation of said check plate relative to said disk.
Claim 2
Dependent Claim
208 words
In a device for securing vanes to a turbine rotor wherein said rotor is a disk having a rim with a plurality of axial grooves on its outer periphery, vanes having roots extending slidably into said grooves and said device comprising at least one annular retaining check plate coaxial with said disk, abutting the ends of said roots, and means for securing said check plate in position, the improvement comprising: said securing means being in the form of radially inwardly extending projections on the radially inner edge of the rim, and generally hook-shaped hangers formed on the radially inner edge of the check plate and engaging said projections to prevent axial movement of said check plate away from said disk, said projections being spaced apart to define indentations for receiving said hangers, said hangers being engageable with and disengageable from said projections by rotating said check plate relative to said disk; elastic tongues defined by cuts extending radially inwardly from the radially outer edge of said check plate; axially extending studs at the outer ends of said tongues, extending toward said disk; and recesses in the adjacent ends of said vanes, said studs extending into said recesses to prevent rotation of said check plate relative to said disk.
Claim 3
Dependent Claim
44 words
A device according to claim 1 wherein each vane includes a platform portion, adjacent said disk, abutting the platform portion of an adjacent vane, each of said recesses being formed partially in each of adjacent platforms whereby said studs each engages two adjacent vanes.
Claim 4
Dependent Claim
16 words
A device according to claim 1 wherein said studs are in radial alignment with said hangers.
Claim 5
Dependent Claim
36 words
A device according to claim 1 including gripping means adjacent the outer ends of said tongues, on the side of said check plate opposite said studs whereby said studs may be selectively withdrawn from said recesses.
Claim 6
Independent Claim
32 words
A device according to any one of the preceding claims wherein said annular check plate has an essentially trapezoidal cross section, its radially outer edge being thinner than its radially inner edge.
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) | 1983-02-18 | 1983-08-20 | 1984-02-19 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1987-02-18 | 1987-08-20 | 1988-02-19 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1991-02-18 | 1991-08-20 | 1992-02-19 | $7700.00 | Window Closed / Lapsed |