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US3997280A Expired / Lapsed US ⏱️ 0.0 years remaining

Stators of axial turbomachines

Assignee: Safran Aircraft Engines SAS
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Filing: 1975-06-19
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Granted: 1976-12-14
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Expires: 1995-06-19
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Abstract

Abstract A stator for turbomachines and especially multistage axial compressors is ovided with stationary vanes having peripheral heels secured to a casing. The casing is constituted by a series of coaxial cylindrical annular sections between which are formed annular spaces for inserting and guiding the heels. The sections are rigidly fixed to ring-shaped peripheral webs or flanges which are secured to each other by means of radial longitudinal ribs.

Inventors

  • 👤 Roger Louis Elysee Germain

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-07 21:27
CPC Classifications
F; F01; F01D; F01D9/00; F01D9/02; F01D9/04; F01D9/042; Y; Y02; Y02T; Y02T50/00; Y02T50/60

Claims Analysis

Total Claims: 9
Claim 1
Independent Claim 145 words
A monoblock stator casing for a multistage axial compressor in which stationary vanes are anchored to the stator casing by peripheral heels, said casing including a series of coaxial cylindrical annular sections which define annular spaces between said sections, heels of said stationary vanes being inserted and circumferentially guided in said spaces, said sections being rigidly fixed to ring-shaped peripheral webs, adjacent ones of said webs being secured to each other by radial longitudinal ribs, said heels of said vanes each having a peripheral end portion of substantially greater width than the corresponding one of said annular spaces and the edges of said end portions being abuttingly engaged by means comprising a centripetal-action clamping device against the ends of the sections which define said space and clearance openings for positioning and sliding of said heels within the annular spaces at the level of said ribs.
Claim 2
Dependent Claim 145 words
A monoblock stator casing for a multistage axial compressor in which stationary vanes are anchored to the stator casing by peripheral heels, said casing including a series of coaxial cylindrical annular sections which define annular spaces between said sections, heels of said stationary vanes being inserted and circumferentially guided in said spaces, said sections being rigidly fixed to ring-shaped peripheral webs, adjacent ones of said webs being secured to each other by radial longitudinal ribs, said heels of said vanes each having a peripheral end portion of substantially greater width than the corresponding one of said annular spaces and the edges of said end portions being abuttingly engaged by means comprising a centripetal-action clamping device against the ends of the sections which define said space and clearance openings for positioning and sliding of said heels within the annular spaces at the level of said ribs.
Claim 3
Dependent Claim 23 words
A stator according to claim 1, wherein said annular sections, said webs and said ribs are joined by molding and also by welding.
Claim 4
Dependent Claim 18 words
A stator according to claim 1, wherein said clamping device is a stretched strap surrounding the stationary-vane heels.
Claim 5
Dependent Claim 18 words
A stator according to claim 1, wherein said clamping device is an articulated chain surrounding the stationary-vane heels.
Claim 6
Dependent Claim 21 words
A stator according to claim 1, wherein said clamping device is a set of wedges and plates surrounding the stationary-vane heels.
Claim 7
Dependent Claim 32 words
A stator according to claim 1, including a seal which surrounds the heel of each vane between the end portion and the annular-section extremities against which the end portion is abuttingly applied.
Claim 8
Dependent Claim 39 words
A stator according to claim 1, said longitudinal ribs having a Y-shaped cross-section wherein the stem of said Y is along the axis of the compressor and the arms of the Y are towards the periphery of the compressor.
Claim 9
Dependent Claim 20 words
A stator according to claim 1, at least a part of the webs and flanges being in a cylindrical sleeve.

References Cited (Backward Citations)

CH234847A Cited
GB572859A Cited
GB599391A Cited
US2489535A Cited
US2995294A Cited
US3105281A Cited
US3339833A Cited
US3241493A Cited
US3291382A Cited
US3393436A Cited
US3326523A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1979-12-14 1980-06-14 1980-12-14 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1983-12-14 1984-06-14 1984-12-14 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1987-12-14 1988-06-14 1988-12-14 $7700.00 Window Closed / Lapsed

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