FR2994216B1 - Partie de revolution de carter intermediaire comportant un insert dispose dans une rainure annulaire - Google Patents
Partie de revolution de carter intermediaire comportant un insert dispose dans une rainure annulaireInfo
- Publication number
- FR2994216B1 FR2994216B1 FR1257539A FR1257539A FR2994216B1 FR 2994216 B1 FR2994216 B1 FR 2994216B1 FR 1257539 A FR1257539 A FR 1257539A FR 1257539 A FR1257539 A FR 1257539A FR 2994216 B1 FR2994216 B1 FR 2994216B1
- Authority
- FR
- France
- Prior art keywords
- carter
- annular groove
- insert disposed
- revolution part
- revolution
- 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.)
- Active
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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/64—Reversing fan flow
- F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/06—Arrangements of bearings; Lubricating
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/28—Arrangement of seals
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/30—Retaining components in desired mutual position
- F05D2260/36—Retaining components in desired mutual position by a form fit connection, e.g. by interlocking
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49316—Impeller making
- Y10T29/4932—Turbomachine making
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1257539A FR2994216B1 (fr) | 2012-08-02 | 2012-08-02 | Partie de revolution de carter intermediaire comportant un insert dispose dans une rainure annulaire |
US13/951,681 US9677425B2 (en) | 2012-08-02 | 2013-07-26 | Axisymmetrical intermediate case part including an insert positioned in an annular groove |
GB1313823.5A GB2507842B (en) | 2012-08-02 | 2013-08-01 | Axisymmetrical Intermediate Case Part Including an Insert positioned in an Annular Groove |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1257539A FR2994216B1 (fr) | 2012-08-02 | 2012-08-02 | Partie de revolution de carter intermediaire comportant un insert dispose dans une rainure annulaire |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2994216A1 FR2994216A1 (fr) | 2014-02-07 |
FR2994216B1 true FR2994216B1 (fr) | 2014-09-05 |
Family
ID=47424998
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1257539A Active FR2994216B1 (fr) | 2012-08-02 | 2012-08-02 | Partie de revolution de carter intermediaire comportant un insert dispose dans une rainure annulaire |
Country Status (3)
Country | Link |
---|---|
US (1) | US9677425B2 (fr) |
FR (1) | FR2994216B1 (fr) |
GB (1) | GB2507842B (fr) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP6118721B2 (ja) * | 2013-12-20 | 2017-04-19 | 株式会社Ihi | ファンケース及びファンケースの製造方法 |
CA2952944A1 (fr) * | 2014-08-22 | 2016-02-25 | Ihi Corporation | Boitier cylindrique |
PL415487A1 (pl) * | 2015-12-31 | 2017-07-03 | General Electric Company | Formowana kompozytowa osłona chroniąca przed zużyciem krawędzi dla złącza w postaci wpustu V-kształtnego i łopatki V-kształtnej |
US10605198B2 (en) * | 2016-04-15 | 2020-03-31 | Rohr, Inc. | Nacelle thrust reverser |
FR3117173A1 (fr) * | 2020-12-09 | 2022-06-10 | Safran Aircraft Engines | Ensemble propulsif d’aéronef et procédé d’adaptation d’un ensemble propulsif |
FR3121709B1 (fr) | 2021-04-08 | 2023-05-05 | Safran Aircraft Engines | Virole extérieure de carter intermédiaire en matériau composite, pour turbomachine d’aéronef |
GB2620735A (en) * | 2022-07-18 | 2024-01-24 | Rolls Royce Plc | Liner for groove of gas turbine engine and method of manufacturing thereof |
Family Cites Families (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1909353A (en) * | 1932-04-20 | 1933-05-16 | James C Harris | Ornament fastener |
US3076634A (en) * | 1959-06-12 | 1963-02-05 | Ass Elect Ind | Locking means for compressor and turbine blades |
US3323807A (en) * | 1964-04-27 | 1967-06-06 | Dana Corp | Piston ring |
US3601415A (en) * | 1970-02-26 | 1971-08-24 | Dana Corp | Piston ring spacer-expander |
US4746129A (en) * | 1987-09-14 | 1988-05-24 | Puccio Guy S | Expansion joint strip seal |
US4998409A (en) * | 1989-09-25 | 1991-03-12 | Rohr Industries, Inc. | Thrust reverser torque ring |
US5749218A (en) * | 1993-12-17 | 1998-05-12 | General Electric Co. | Wear reduction kit for gas turbine combustors |
FR2732074B1 (fr) * | 1995-03-21 | 1997-06-06 | Aerospatiale | Turboreacteur a double flux a nacelle flottante |
FR2756323B1 (fr) * | 1996-11-28 | 1998-12-31 | Hispano Suiza Sa | Dispositif de liaison d'un inverseur de poussee a un turbomoteur |
US6431835B1 (en) * | 2000-10-17 | 2002-08-13 | Honeywell International, Inc. | Fan blade compliant shim |
US7399159B2 (en) * | 2003-06-25 | 2008-07-15 | Florida Turbine Technologies, Inc | Detachable leading edge for airfoils |
DE102004006706A1 (de) * | 2004-02-11 | 2005-08-25 | Mtu Aero Engines Gmbh | Dämpfungsanordnung für Leifschaufeln |
FR2869290B1 (fr) * | 2004-04-27 | 2006-07-21 | Hurel Hispano Sa | Groupe turbopropulseur pour aeronef a installation aerodynamique amelioree |
GB2429043B (en) * | 2005-08-13 | 2008-02-13 | Rolls Royce Plc | Clip |
US7360988B2 (en) * | 2005-12-08 | 2008-04-22 | General Electric Company | Methods and apparatus for assembling turbine engines |
US7784264B2 (en) * | 2006-08-03 | 2010-08-31 | Siemens Energy, Inc. | Slidable spring-loaded transition-to-turbine seal apparatus and heat-shielding system, comprising the seal, at transition/turbine junction of a gas turbine engine |
US9643286B2 (en) * | 2007-04-05 | 2017-05-09 | United Technologies Corporation | Method of repairing a turbine engine component |
FR2925120B1 (fr) * | 2007-12-18 | 2010-02-19 | Snecma | Extension de carter intermediaire pour turboreacteur d'aeronef, comprenant une rainure annulaire sectorisee de reception des capots de nacelle |
GB0807137D0 (en) * | 2008-04-21 | 2008-05-21 | Rolls Royce Plc | Rear fan case for a gas turbine engine |
US8511969B2 (en) * | 2009-10-01 | 2013-08-20 | Pratt & Whitney Canada Corp. | Interturbine vane with multiple air chambers |
GB2477825B (en) * | 2010-09-23 | 2015-04-01 | Rolls Royce Plc | Anti fret liner assembly |
EP2442032A1 (fr) * | 2010-10-12 | 2012-04-18 | Siemens Aktiengesellschaft | Segment d'usure dans l'accrochage de support d'aube directrice de turbines d'une coque extérieure d'une chambre de combustion annulaire |
FR2986836B1 (fr) * | 2012-02-09 | 2016-01-01 | Snecma | Tole annulaire anti-usure pour une turbomachine |
FR2990001B1 (fr) * | 2012-04-27 | 2016-01-08 | Snecma | Assemblage d'un echangeur thermique au sein d'un carter intermediaire de turboreacteur |
US9500083B2 (en) * | 2012-11-26 | 2016-11-22 | U.S. Department Of Energy | Apparatus and method to reduce wear and friction between CMC-to-metal attachment and interface |
-
2012
- 2012-08-02 FR FR1257539A patent/FR2994216B1/fr active Active
-
2013
- 2013-07-26 US US13/951,681 patent/US9677425B2/en active Active
- 2013-08-01 GB GB1313823.5A patent/GB2507842B/en active Active
Also Published As
Publication number | Publication date |
---|---|
GB2507842A (en) | 2014-05-14 |
GB201313823D0 (en) | 2013-09-18 |
US20140294573A1 (en) | 2014-10-02 |
GB2507842B (en) | 2019-11-27 |
US9677425B2 (en) | 2017-06-13 |
FR2994216A1 (fr) | 2014-02-07 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
FR2997746B1 (fr) | Ensemble de soupape | |
FR2997726B1 (fr) | Carter de turbomachine | |
BR112014032111A2 (pt) | unidade de digestão. | |
BR302013000792S1 (pt) | Alojamento de lâmpada. | |
FR2994216B1 (fr) | Partie de revolution de carter intermediaire comportant un insert dispose dans une rainure annulaire | |
BR112014024484A2 (pt) | interação com serviço confiável | |
FR2997444B1 (fr) | Moyeu de carter pour une turbomachine | |
BR302012005910S1 (pt) | Configuração aplicada em farol para motocicleta. | |
EP2804787A4 (fr) | Assemblage de boîte d'écrasement sinusoïdale | |
FR2997725B1 (fr) | Carter de turbomachine | |
FR2995949B1 (fr) | Carter de turbomachine | |
FR3005099B1 (fr) | Structure de turbomachine comportant une bague de ventilation | |
ITTO20130048A1 (it) | Motociclo. | |
DE112013004558A5 (de) | Dichtungsanordnung | |
BR112015009171A2 (pt) | conjunto de cabeça de poço | |
FR2993954B1 (fr) | Vanne motorisee comportant une douille instrumentee. | |
FR2992527B3 (fr) | Sous-vetement de securite | |
FR2987595B1 (fr) | Trottinette. | |
EP2864547A4 (fr) | Collecteur d'huile | |
BR112014029893A2 (pt) | encaixe de tubulação. | |
FR2995660B1 (fr) | Luminaire de securite encastre | |
GB201312327D0 (en) | Engine assembly | |
DE112013002624A5 (de) | Fahrradscheinwerfer | |
ES1078881Y (es) | Cubo de basura | |
FR2998032B1 (fr) | Lanterne |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PLFP | Fee payment |
Year of fee payment: 5 |
|
PLFP | Fee payment |
Year of fee payment: 6 |
|
CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170719 |
|
PLFP | Fee payment |
Year of fee payment: 7 |
|
PLFP | Fee payment |
Year of fee payment: 8 |
|
PLFP | Fee payment |
Year of fee payment: 9 |
|
PLFP | Fee payment |
Year of fee payment: 10 |
|
PLFP | Fee payment |
Year of fee payment: 11 |
|
PLFP | Fee payment |
Year of fee payment: 12 |