FR2282537A1 - Perfectionnements aux carters de turbomoteurs - Google Patents
Perfectionnements aux carters de turbomoteursInfo
- Publication number
- FR2282537A1 FR2282537A1 FR7525907A FR7525907A FR2282537A1 FR 2282537 A1 FR2282537 A1 FR 2282537A1 FR 7525907 A FR7525907 A FR 7525907A FR 7525907 A FR7525907 A FR 7525907A FR 2282537 A1 FR2282537 A1 FR 2282537A1
- Authority
- FR
- France
- Prior art keywords
- turbomotor
- casings
- turbomotor casings
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24149—Honeycomb-like
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/30—Self-sustaining carbon mass or layer with impregnant or other layer
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB37041/74A GB1485032A (en) | 1974-08-23 | 1974-08-23 | Gas turbine engine casing |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2282537A1 true FR2282537A1 (fr) | 1976-03-19 |
FR2282537B1 FR2282537B1 (fr) | 1979-09-07 |
Family
ID=10393268
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7525907A Granted FR2282537A1 (fr) | 1974-08-23 | 1975-08-21 | Perfectionnements aux carters de turbomoteurs |
Country Status (6)
Country | Link |
---|---|
US (1) | US4063847A (fr) |
JP (1) | JPS5146610A (fr) |
DE (1) | DE2536514A1 (fr) |
FR (1) | FR2282537A1 (fr) |
GB (1) | GB1485032A (fr) |
IT (1) | IT1044585B (fr) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2470269A1 (fr) * | 1979-11-27 | 1981-05-29 | Snecma | Structure de retention pour carter de compresseur d'une turbomachine |
DE3827680A1 (de) * | 1988-08-16 | 1990-02-22 | Mtu Muenchen Gmbh | Einrichtung zur befestigung eines aus titan gefertigten leitgitters eines axialverdichters an einem aus einem faserverstaerkten kunststoff gefertigten verdichtergehaeuse |
EP2811121A1 (fr) | 2013-06-03 | 2014-12-10 | Techspace Aero S.A. | Carter composite de compresseur de turbomachine axiale avec bride de fixation métallique |
Families Citing this family (54)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS5757983Y2 (fr) * | 1977-05-12 | 1982-12-11 | ||
FR2444800A1 (fr) * | 1978-12-21 | 1980-07-18 | Rolls Royce | Anneau de retenue pour moteur a turbine a gaz |
JPS5731073Y2 (fr) * | 1979-01-17 | 1982-07-08 | ||
JPS55132284A (en) * | 1979-04-03 | 1980-10-14 | Ricoh Co Ltd | Thermal head |
FR2467978A1 (fr) * | 1979-10-23 | 1981-04-30 | Snecma | Dispositif de retention pour carter de compresseur d'une turbomachine |
GB2095749B (en) * | 1981-03-25 | 1984-12-12 | Rolls Royce | Gas turbine engine having improved resistance for foreign object ingestion damage |
US4452564A (en) * | 1981-11-09 | 1984-06-05 | The Garrett Corporation | Stator vane assembly and associated methods |
US4718818A (en) * | 1981-12-21 | 1988-01-12 | United Technologies Corporation | Containment structure |
US4475864A (en) * | 1981-12-21 | 1984-10-09 | United Technologies Corporation | Containment structure |
US4452565A (en) * | 1981-12-21 | 1984-06-05 | United Technologies Corporation | Containment structure |
FR2547357A1 (fr) * | 1983-06-09 | 1984-12-14 | Snecma | Structure de retention pour carter de turbomachine |
FR2574476B1 (fr) * | 1984-12-06 | 1987-01-02 | Snecma | Carter de retention pour soufflante de turboreacteur |
FR2575699B1 (fr) * | 1985-01-09 | 1987-05-22 | Dassault Avions | Capots resistant au feu, en particulier pour moteurs d'avions |
US5054281A (en) * | 1989-09-25 | 1991-10-08 | Rohr Industries, Inc. | Gas turbine engine compartment vent system |
US5226789A (en) * | 1991-05-13 | 1993-07-13 | General Electric Company | Composite fan stator assembly |
US5447411A (en) * | 1993-06-10 | 1995-09-05 | Martin Marietta Corporation | Light weight fan blade containment system |
US5771680A (en) * | 1995-12-21 | 1998-06-30 | General Electric Company | Stiffened composite structures and method of making thereof |
DE19833604A1 (de) * | 1997-07-29 | 1999-02-04 | Luk Fahrzeug Hydraulik | Kompressor |
US6206631B1 (en) * | 1999-09-07 | 2001-03-27 | General Electric Company | Turbomachine fan casing with dual-wall blade containment structure |
US6341938B1 (en) * | 2000-03-10 | 2002-01-29 | General Electric Company | Methods and apparatus for minimizing thermal gradients within turbine shrouds |
FR2819026B1 (fr) * | 2001-01-04 | 2003-02-28 | Snecma Moteurs | Stator de compresseur axial de turbine a gaz |
US6892931B2 (en) * | 2002-12-27 | 2005-05-17 | General Electric Company | Methods for replacing portions of turbine shroud supports |
US7094029B2 (en) * | 2003-05-06 | 2006-08-22 | General Electric Company | Methods and apparatus for controlling gas turbine engine rotor tip clearances |
EP1649145B1 (fr) * | 2003-07-29 | 2008-05-28 | Pratt & Whitney Canada Corp. | Carter de turbofan, moteur turbofan et procédé associé |
US7370467B2 (en) * | 2003-07-29 | 2008-05-13 | Pratt & Whitney Canada Corp. | Turbofan case and method of making |
GB0403941D0 (en) * | 2004-02-21 | 2004-03-24 | Rolls Royce Plc | A gas turbine engine blade containment assembly |
US20080152853A1 (en) * | 2006-12-21 | 2008-06-26 | Lee Alan Blanton | Composite containment casings for turbine engine and methods for fabricating the same |
FR2913053B1 (fr) * | 2007-02-23 | 2009-05-22 | Snecma Sa | Procede de fabrication d'un carter de turbine a gaz en materiau composite et carter ainsi obtenu |
US7897241B2 (en) * | 2009-02-26 | 2011-03-01 | Rolls-Royce Corporation | Composite spacer |
US8177494B2 (en) | 2009-03-15 | 2012-05-15 | United Technologies Corporation | Buried casing treatment strip for a gas turbine engine |
US8469661B2 (en) * | 2009-10-01 | 2013-06-25 | Pratt & Whitney Canada Corp. | Fabricated gas turbine vane ring |
US20110146944A1 (en) * | 2009-12-22 | 2011-06-23 | John Hand | Heat Exchanger Mounting Assembly |
US8510945B2 (en) * | 2009-12-22 | 2013-08-20 | Unison Industries, Llc | Method of mounting a heat exchanger in a gas turbine engine assembly |
EP2418387B1 (fr) * | 2010-08-11 | 2015-04-01 | Techspace Aero S.A. | Virole externe de compresseur de turbomachine axiale |
US8858156B2 (en) * | 2010-08-12 | 2014-10-14 | General Electric Company | Fragment containment assembly and method for adding a fragment containment assembly to a turbine |
US9126374B2 (en) | 2010-09-28 | 2015-09-08 | Russell B. Hanson | Iso-grid composite component |
US20120082556A1 (en) * | 2010-09-30 | 2012-04-05 | Enzo Macchia | Nanocrystalline metal coated composite airfoil |
US9587645B2 (en) | 2010-09-30 | 2017-03-07 | Pratt & Whitney Canada Corp. | Airfoil blade |
US9429029B2 (en) | 2010-09-30 | 2016-08-30 | Pratt & Whitney Canada Corp. | Gas turbine blade and method of protecting same |
US20120082553A1 (en) * | 2010-09-30 | 2012-04-05 | Andreas Eleftheriou | Metal encapsulated stator vane |
US20120082541A1 (en) * | 2010-09-30 | 2012-04-05 | Enzo Macchia | Gas turbine engine casing |
US8889263B2 (en) | 2010-12-30 | 2014-11-18 | Rolls-Royce Corporation | Composite structure |
GB2489673B (en) * | 2011-03-29 | 2015-08-12 | Rolls Royce Plc | A containment casing for a gas turbine engine |
US8801376B2 (en) | 2011-09-02 | 2014-08-12 | Pratt & Whitney Canada Corp. | Fabricated intermediate case with engine mounts |
US9427835B2 (en) | 2012-02-29 | 2016-08-30 | Pratt & Whitney Canada Corp. | Nano-metal coated vane component for gas turbine engines and method of manufacturing same |
US9528391B2 (en) | 2012-07-17 | 2016-12-27 | United Technologies Corporation | Gas turbine engine outer case with contoured bleed boss |
US9556746B2 (en) | 2013-10-08 | 2017-01-31 | Pratt & Whitney Canada Corp. | Integrated strut and turbine vane nozzle arrangement |
US9598981B2 (en) * | 2013-11-22 | 2017-03-21 | Siemens Energy, Inc. | Industrial gas turbine exhaust system diffuser inlet lip |
EP2883688B1 (fr) * | 2013-12-13 | 2021-09-22 | Safran Aero Boosters SA | Carter annulaire composite de compresseur de turbomachine et procédé d'obtention de celui-ci |
EP2960437B1 (fr) * | 2014-06-26 | 2018-08-08 | MTU Aero Engines GmbH | Système d'aubes de guidage variables pour une turbine à gaz et turbine à gaz dotée d'un tel système |
JP6271077B2 (ja) | 2014-07-24 | 2018-01-31 | シーメンス アクチエンゲゼルシヤフトSiemens Aktiengesellschaft | ガスタービンエンジン内で使用可能なステータベーンシステム |
DE102016213813A1 (de) * | 2016-07-27 | 2018-02-01 | MTU Aero Engines AG | Verkleidungselement einer Strömungsmaschine und entsprechende Verbindungsanordnung |
US10550718B2 (en) | 2017-03-31 | 2020-02-04 | The Boeing Company | Gas turbine engine fan blade containment systems |
US10487684B2 (en) | 2017-03-31 | 2019-11-26 | The Boeing Company | Gas turbine engine fan blade containment systems |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB660383A (en) * | 1949-02-23 | 1951-11-07 | Winnett Boyd | Blade mounting for axial-flow compressors and the like |
US2834537A (en) * | 1954-01-18 | 1958-05-13 | Ryan Aeronautical Co | Compressor stator structure |
US2995294A (en) * | 1954-12-02 | 1961-08-08 | Studebaker Packard Corp | Stator casing and blade assembly |
US3013641A (en) * | 1957-04-29 | 1961-12-19 | Thompson Ramo Wooldridge Inc | Structural element |
US3279967A (en) * | 1961-04-07 | 1966-10-18 | Carrier Corp | Method of fabricating a rotor shroud |
GB995228A (en) * | 1964-05-08 | 1965-06-16 | Rolls Royce | Bladed structure, for example, for a gas turbine engine compressor |
GB1054608A (fr) * | 1965-09-16 | |||
GB1118898A (en) * | 1967-04-03 | 1968-07-03 | Rolls Royce | Fluid flow machine |
US3514238A (en) * | 1968-09-16 | 1970-05-26 | Black & Decker Mfg Co | Cylinder for fluid pump motor and the like and method of making |
US3556675A (en) * | 1969-01-29 | 1971-01-19 | Gen Electric | Turbomachinery rotor with integral shroud |
FR2143561B1 (fr) * | 1971-06-29 | 1974-03-08 | Snecma | |
US3876327A (en) * | 1973-02-26 | 1975-04-08 | Goulds Pumps | Non-metallic pump |
-
1974
- 1974-08-23 GB GB37041/74A patent/GB1485032A/en not_active Expired
-
1975
- 1975-08-11 US US05/603,606 patent/US4063847A/en not_active Expired - Lifetime
- 1975-08-14 IT IT7526370A patent/IT1044585B/it active
- 1975-08-16 DE DE19752536514 patent/DE2536514A1/de active Pending
- 1975-08-21 FR FR7525907A patent/FR2282537A1/fr active Granted
- 1975-08-23 JP JP50102512A patent/JPS5146610A/ja active Pending
Non-Patent Citations (1)
Title |
---|
NEANT * |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2470269A1 (fr) * | 1979-11-27 | 1981-05-29 | Snecma | Structure de retention pour carter de compresseur d'une turbomachine |
EP0030179A1 (fr) * | 1979-11-27 | 1981-06-10 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." | Structure de rétention pour carter de compresseur d'une turbomachine |
DE3827680A1 (de) * | 1988-08-16 | 1990-02-22 | Mtu Muenchen Gmbh | Einrichtung zur befestigung eines aus titan gefertigten leitgitters eines axialverdichters an einem aus einem faserverstaerkten kunststoff gefertigten verdichtergehaeuse |
EP2811121A1 (fr) | 2013-06-03 | 2014-12-10 | Techspace Aero S.A. | Carter composite de compresseur de turbomachine axiale avec bride de fixation métallique |
Also Published As
Publication number | Publication date |
---|---|
FR2282537B1 (fr) | 1979-09-07 |
JPS5146610A (en) | 1976-04-21 |
US4063847A (en) | 1977-12-20 |
IT1044585B (it) | 1980-03-31 |
GB1485032A (en) | 1977-09-08 |
DE2536514A1 (de) | 1976-03-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CA | Change of address | ||
CD | Change of name or company name | ||
ST | Notification of lapse |