US4411589A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Retaining device for the compressor casing of a turbine engine
Assignee: Safran Aircraft Engines SAS
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Filing: 1980-10-21
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Granted: 1983-10-25
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Expires: 2000-10-21
Abstract
Abstract A ferrule surrounding the blading of a rotor is lined externally with an assembly of elements of revolution. These elements are in the form of cylindrical rings, circular rings or of tori supported between blocking elements. The assembly is formed by alternating rings made of a composite or metallic material and a winding of fibers encased in a polymerizable resin.
Inventors
- 👤 Raymond J. M. Joubert
- 👤 Marcel R. Soligny
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-05 08:39
CPC Classifications
F; F01; F01D; F01D21/00; F01D21/04; F01D21/045; F05; F05D; F05D2220/00; F05D2220/30; F05D2220/32; F05D2220/327; Y; Y02; Y02T; Y02T50/00; Y02T50/60
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
162 words
A retaining device for the compressor casing of a dual flow turbo-jet engine having a metal ferrule coaxial with the axis of the compressor, the metal ferrule having on its internal surface facing the tips of the blades a material capable of entering into non-destructive contact with the tips of the blades, wherein the retaining device comprises: a plurality of first circular rings disposed about the external surface of the ferrule such that their axes coincide with the axis of the compressor, the first circular rings of material capable of frictionally amortizing the kinetic energy of a blade or blade fragment coming into contact therewith; and, a plurality of second circular rings disposed coaxially with the first circular rings and located between each of the first rings such that the first and second rings alternate in a direction along the axis of the compressor, the second circular rings being formed of a high-strength material different from the material forming the first rings.
Claim 2
Dependent Claim
162 words
A retaining device for the compressor casing of a dual flow turbo-jet engine having a metal ferrule coaxial with the axis of the compressor, the metal ferrule having on its internal surface facing the tips of the blades a material capable of entering into non-destructive contact with the tips of the blades, wherein the retaining device comprises: a plurality of first circular rings disposed about the external surface of the ferrule such that their axes coincide with the axis of the compressor, the first circular rings of material capable of frictionally amortizing the kinetic energy of a blade or blade fragment coming into contact therewith; and, a plurality of second circular rings disposed coaxially with the first circular rings and located between each of the first rings such that the first and second rings alternate in a direction along the axis of the compressor, the second circular rings being formed of a high-strength material different from the material forming the first rings.
Claim 3
Dependent Claim
40 words
The retaining device for a compressor casing set forth in claim 1 wherein the dimensions of the first and second rings in a direction along the longitudinal axis of the compressor are smaller than their dimensions in a radial direction.
Claim 4
Dependent Claim
53 words
The retaining device for a compressor casing set forth in claim 2 wherein the internal diameters of the first and second rings are approximately equal to the external diameter of the ferrule, and the external diameters of the first and second rings are substantially smaller than the internal diameter of the compressor casing.
Claim 5
Dependent Claim
28 words
The retaining device for a compressor casing set forth in claim 3 wherein the first rings are formed of polyimide fibers encased in a matrix of polymerizable resin.
Claim 6
Dependent Claim
22 words
The retaining device for a compressor casing set forth in claim 4 wherein the second rings are formed of a composite material.
Claim 7
Dependent Claim
24 words
The retaining device for a compressor casing set forth in claim 5 wherein the first and second rings are adhesively bonded to each other.
Claim 8
Dependent Claim
25 words
The retaining device for a compressor casing set forth in claim 6 wherein the first and second rings are joined to each other by vulcanizing.
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) | 1986-10-24 | 1987-04-25 | 1987-10-25 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1990-10-24 | 1991-04-25 | 1991-10-25 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1994-10-24 | 1995-04-25 | 1995-10-25 | $7700.00 | Window Closed / Lapsed |