Patent US5096377A successfully refreshed from Google Patents.
US5096377A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Turboshaft engine casing joint with reinforced axial restraint
Assignee: Safran Aircraft Engines SAS
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Filing: 1990-12-12
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Granted: 1992-03-17
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Expires: 2010-12-12
Abstract
Abstract The casing of a turboshaft engine, particularly a turbojet engine with a high speed propeller, comprises axially successive shells which are fixed firmly to each other end to end by bolted coupling flanges, at least one of the shells comprising an additional mechanical axial retaining joint enabling the connection between the shells to withstand any exceptional stresses such as those caused by the loss of a propeller blade of the turbojet engine. Preferably the retaining joint comprises a radially inwardly directed tongue carried by one of the shells and received in a radially outwardly open groove provided in a portion of the other shell or a member securely fixed thereto.
Inventors
- 👤 Philippe P. Catte
- 👤 Jacky Naudet
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 21:31
CPC Classifications
F; F04; F04D; F04D29/00; F04D29/40; F04D29/52; F04D29/522; F01; F01D; F01D25/00; F01D25/24; F01D25/26; F01D25/265; F16; F16B; F16B2200/00; F16B2200/30; F16B2200/50; F16B2200/506; Y; Y02; Y02T; Y02T50/00; Y02T50/60
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
68 words
A turboshaft engine casing including axially successive shells, coupling flanges on said shells, and screw-threaded means connecting said coupling flanges to fix said shells firmly to each other end to end, at least one of said shells comprising additional mechanical axial retaining means enabling the connection between said shells to withstand any exceptional mechanical stresses such as those caused by the loss of a propeller of the engine.
Claim 2
Dependent Claim
68 words
A turboshaft engine casing including axially successive shells, coupling flanges on said shells, and screw-threaded means connecting said coupling flanges to fix said shells firmly to each other end to end, at least one of said shells comprising additional mechanical axial retaining means enabling the connection between said shells to withstand any exceptional mechanical stresses such as those caused by the loss of a propeller of the engine.
Claim 3
Dependent Claim
47 words
A casing in accordance with claim 1, wherein said axial retaining means comprises a radially inwardly directed tongue carried by said coupling flange of one of said shells, and a portion of said other shell provided with a radially outwardly open groove which receives said tongue therein.
Claim 4
Dependent Claim
54 words
A casing in accordance with claim 1, wherein said axial retaining means comprises a radially inwardly directed tongue carried by said coupling flange of one of said shells, and a member which is secured firmly to said other shell, said member being provided with a radially outwardly open groove which receives said tongue therein.
Claim 5
Dependent Claim
70 words
A casing in accordance with claim 3, wherein there is a radially inwardly directed tongue carried by said coupling flange of each of said shells, and said member comprises an intermediate flange sandwiched between said coupling flanges, said member being provided with two radially outwardly open grooves, one of said grooves receiving said tongue on one of said shells, and said other groove receiving said tongue on said other shell.
Claim 6
Dependent Claim
13 words
A casing in accordance with claim 1, wherein said shells are semi-circular shells.
Claim 7
Dependent Claim
80 words
A casing in accordance with claim 2 or claim 3, wherein said shells are circular, and said groove and said tongue each comprise cut-out sections at circumferentially spaced intervals so as to permit said tongue to be fitted into said groove by relative axial movement of said shells to move said tongue into the cut-out sections of said groove followed by relative rotation of said shells to move said tongue into said groove before said coupling flanges are connected together.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1995-03-17 | 1995-09-16 | 1996-03-17 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1999-03-17 | 1999-09-16 | 2000-03-17 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2003-03-17 | 2003-09-16 | 2004-03-17 | $7700.00 | Window Closed / Lapsed |