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US4222706A Expired / Lapsed US ⏱️ 0.0 years remaining

Porous abradable shroud with transverse partitions

Assignee: Safran Aircraft Engines SAS
•
Filing: 1978-08-01
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Granted: 1980-09-16
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Expires: 1998-08-01
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Abstract

Abstract A turbine housing for a jet engine is provided with a ring of an abradableorous material. A supporting and mounting device consisting of a cylindricoconical monoblock having a conical internal jacket provides for the convection cooling of the external surface and a cylindrical jacket for cooling air is held over the abradable ring by means of a perforated ferrule integral with the rest of the device. The abradable ring carries transverse partitions to prevent axial leakage.

Inventors

  • 👤 Michel R. Ayache
  • 👤 Pierre A. Glowacki
  • 👤 Gerard M. F. Mandet

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-30 15:52
CPC Classifications
F; F01; F01D; F01D11/00; F01D11/08

Claims Analysis

Total Claims: 11
Claim 1
Independent Claim 65 words
In a housing for a jet engine having turbine blades in said housing and a ring including an abradable portion of a sintered porous material surrounding said turbine blades and wherein said ring is cooled by transpiration of air therethrough, the improvement comprising: said ring being provided with partitions within the material of the ring and extending therethrough transverse to the axis of said rotor.
Claim 2
Dependent Claim 65 words
In a housing for a jet engine having turbine blades in said housing and a ring including an abradable portion of a sintered porous material surrounding said turbine blades and wherein said ring is cooled by transpiration of air therethrough, the improvement comprising: said ring being provided with partitions within the material of the ring and extending therethrough transverse to the axis of said rotor.
Claim 3
Dependent Claim 25 words
A housing as defined in claim 1 wherein at least portions of said partitions are oriented obliquely with respect to the axis of said rotor.
Claim 4
Dependent Claim 26 words
A housing as defined in claim 1 wherein the partitions through said sintered material are zones of the material of said ring fused by electron bombardment.
Claim 5
Dependent Claim 34 words
A housing as defined in claim 1 wherein said sintered material is provided on its inner face with grooves at the ends of said partitions, said grooves being adjacent the apexes of said blades.
Claim 6
Dependent Claim 96 words
A housing as defined in claim 1 wherein said housing comprises a monoblock structure of a cylindroconical revolution, having an external cylindrical portion carrying means for securing it to the engine, a conical portion extending from said external cylindrical portion, a perforated cylindrical ferrule secured to the inside of the external conical part at one end and constituting a portion of said ring supporting said sintered material, a conical jacket secured by spacers to the inside of the external conical part and spaced inwardly therefrom, and a perforated cylindrical jacket secured by spacers over said ferrule.
Claim 7
Dependent Claim 18 words
A housing as defined in claim 5 wherein said last-named spacers consist of radial ribs on said ferrule.
Claim 8
Dependent Claim 20 words
A housing as defined in claim 5 wherein said last-named spacers consist of radial ribs on said perforated cylindrical jacket.
Claim 9
Dependent Claim 21 words
A housing as defined in claim 6 wherein said ribs are secured to the sintered material in line with its partitions.
Claim 10
Dependent Claim 21 words
A housing as defined in claim 5 wherein the perforations of said ferrule extend oblique to the axis of said rotor.
Claim 11
Dependent Claim 13 words
A housing as defined in claim 5 wherein said first-named spacers are spheres.

References Cited (Backward Citations)

US3126149A Cited
US3146992A Cited
US3365172A Cited
US3728039A Cited
US3656862A Cited
US3825364A Cited
US3834001A Cited
US3825365A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1983-09-16 1984-03-17 1984-09-16 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1987-09-16 1988-03-17 1988-09-16 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1991-09-16 1992-03-17 1992-09-16 $7700.00 Window Closed / Lapsed

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