BR112014026258A2 - conjunto de recipiente, método para montar um conjunto de recipiente e motor de turbina a gás - Google Patents
conjunto de recipiente, método para montar um conjunto de recipiente e motor de turbina a gásInfo
- Publication number
- BR112014026258A2 BR112014026258A2 BR112014026258A BR112014026258A BR112014026258A2 BR 112014026258 A2 BR112014026258 A2 BR 112014026258A2 BR 112014026258 A BR112014026258 A BR 112014026258A BR 112014026258 A BR112014026258 A BR 112014026258A BR 112014026258 A2 BR112014026258 A2 BR 112014026258A2
- Authority
- BR
- Brazil
- Prior art keywords
- container
- assembly
- mounting
- gas turbine
- engine
- Prior art date
Links
Classifications
-
- 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
- F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
-
- 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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
- F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
-
- 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
- F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
-
- 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
- F01D9/00—Stators
- F01D9/06—Fluid supply conduits to nozzles or the like
- F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
-
- 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
- F02C7/32—Arrangement, mounting, or driving, of auxiliaries
-
- 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
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
-
- 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
- Y10T29/49229—Prime mover or fluid pump making
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Motor Power Transmission Devices (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201261637954P | 2012-04-25 | 2012-04-25 | |
PCT/US2013/037270 WO2014018137A2 (en) | 2012-04-25 | 2013-04-19 | Aircraft engine driveshaft vessel assembly and method of assembling the same |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112014026258A2 true BR112014026258A2 (pt) | 2017-06-27 |
Family
ID=49517623
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112014026258A BR112014026258A2 (pt) | 2012-04-25 | 2013-04-19 | conjunto de recipiente, método para montar um conjunto de recipiente e motor de turbina a gás |
Country Status (7)
Country | Link |
---|---|
US (1) | US9657646B2 (pt) |
EP (1) | EP2841712A2 (pt) |
JP (1) | JP5856711B2 (pt) |
CN (1) | CN104350237B (pt) |
BR (1) | BR112014026258A2 (pt) |
CA (1) | CA2870669A1 (pt) |
WO (1) | WO2014018137A2 (pt) |
Families Citing this family (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3022301B1 (fr) * | 2014-06-12 | 2016-07-29 | Snecma | Turbomachine comprenant un systeme d'entrainement d'un equipement tel qu'un boitier d'accessoires |
US9915225B2 (en) * | 2015-02-06 | 2018-03-13 | United Technologies Corporation | Propulsion system arrangement for turbofan gas turbine engine |
FR3039598B1 (fr) | 2015-07-29 | 2019-12-27 | Safran Aircraft Engines | Ensemble de redressement de flux d'air a performances aerodynamiques ameliorees |
EP3246528B1 (en) | 2016-05-18 | 2020-10-28 | Rolls-Royce Corporation | Low pressure generator with electrical assembly for gas turbine engine |
DE102016215030A1 (de) * | 2016-08-11 | 2018-02-15 | Rolls-Royce Deutschland Ltd & Co Kg | Turbofan-Triebwerk mit einer im Sekundärstromkanal liegenden und ein separates Abschlusselement aufweisenden Verkleidung |
US11022042B2 (en) | 2016-08-29 | 2021-06-01 | Rolls-Royce North American Technologies Inc. | Aircraft having a gas turbine generator with power assist |
US10654577B2 (en) * | 2017-02-22 | 2020-05-19 | General Electric Company | Rainbow flowpath low pressure turbine rotor assembly |
US11255215B2 (en) | 2017-07-06 | 2022-02-22 | Rolls-Royce North American Technologies Inc. | Gas turbine engine with microchannel cooled electric device |
FR3071868B1 (fr) * | 2017-10-02 | 2019-09-27 | Safran Aircraft Engines | Bras pour carter de turbomachine comprenant un corps et une piece amovible |
FR3090033B1 (fr) * | 2018-12-18 | 2020-11-27 | Safran Aircraft Engines | Ensemble d’aube directrice de sortie et de bifurcation pour turbomachine |
US10823006B2 (en) * | 2019-03-14 | 2020-11-03 | Raytheon Technologies Corporation | Lubrication systems and methods with superposition gearbox |
Family Cites Families (23)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB926947A (en) * | 1961-11-27 | 1963-05-22 | Rolls Royce | Improvements relating to gas turbine engine casings |
US4722666A (en) | 1987-06-29 | 1988-02-02 | United Technologies Corporation | Nose cowl mounted oil lubricating and cooling system |
US5080555A (en) | 1990-11-16 | 1992-01-14 | General Motors Corporation | Turbine support for gas turbine engine |
AU666211B2 (en) | 1992-06-22 | 1996-02-01 | United Technologies Corporation | Toroidal fuselage for unmanned aerial vehicle |
GB9606546D0 (en) | 1996-03-28 | 1996-06-05 | Rolls Royce Plc | Gas turbine engine system |
US6195983B1 (en) | 1999-02-12 | 2001-03-06 | General Electric Company | Leaned and swept fan outlet guide vanes |
JP2002081326A (ja) | 2000-09-05 | 2002-03-22 | Ishikawajima Harima Heavy Ind Co Ltd | 航空機用エンジンのラジアルドライブシャフト中間支持装置 |
JP4192661B2 (ja) | 2003-04-14 | 2008-12-10 | 株式会社Ihi | ガスタービンの垂直軸の支持構造 |
GB0315894D0 (en) | 2003-07-08 | 2003-08-13 | Rolls Royce Plc | Aircraft engine arrangement |
US7233295B2 (en) | 2005-05-03 | 2007-06-19 | Florenio Pinili Regala | Conformal driveshaft cover SATCOM antenna |
US7500365B2 (en) * | 2005-05-05 | 2009-03-10 | United Technologies Corporation | Accessory gearbox |
GB0520850D0 (en) * | 2005-10-14 | 2005-11-23 | Rolls Royce Plc | Fan static structure |
US7607308B2 (en) | 2005-12-08 | 2009-10-27 | General Electric Company | Shrouded turbofan bleed duct |
GB0608983D0 (en) | 2006-05-06 | 2006-06-14 | Rolls Royce Plc | Aeroengine mount |
FR2907167B1 (fr) | 2006-10-13 | 2011-11-18 | Snecma | Arbre d'entrainement de boitier a engrenages de machines auxiliaires d'un turboreacteur; machine auxiliaire supplementaire modulaire |
US20080159851A1 (en) | 2006-12-29 | 2008-07-03 | Thomas Ory Moniz | Guide Vane and Method of Fabricating the Same |
FR2921973B1 (fr) | 2007-10-04 | 2011-04-29 | Snecma | Carter intermediaire de turboreacteur et turboreacteur |
GB0719786D0 (en) * | 2007-10-11 | 2007-11-21 | Rolls Royce Plc | A vane and a vane assembly for a gas turbine engine |
US8221071B2 (en) * | 2008-09-30 | 2012-07-17 | General Electric Company | Integrated guide vane assembly |
US9121351B2 (en) * | 2008-10-30 | 2015-09-01 | Rolls-Royce North American Technologies, Inc. | Gas turbine engine accessory system |
US8661781B2 (en) * | 2009-02-13 | 2014-03-04 | The Boeing Company | Counter rotating fan design and variable blade row spacing optimization for low environmental impact |
US8514136B2 (en) | 2009-10-26 | 2013-08-20 | The Boeing Company | Conformal high frequency antenna |
US9297312B2 (en) * | 2012-12-29 | 2016-03-29 | United Technologies Corporation | Circumferentially retained fairing |
-
2013
- 2013-04-19 JP JP2015507199A patent/JP5856711B2/ja not_active Expired - Fee Related
- 2013-04-19 EP EP13785968.2A patent/EP2841712A2/en not_active Withdrawn
- 2013-04-19 BR BR112014026258A patent/BR112014026258A2/pt not_active IP Right Cessation
- 2013-04-19 US US14/395,879 patent/US9657646B2/en active Active
- 2013-04-19 CN CN201380021840.XA patent/CN104350237B/zh active Active
- 2013-04-19 CA CA2870669A patent/CA2870669A1/en not_active Abandoned
- 2013-04-19 WO PCT/US2013/037270 patent/WO2014018137A2/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
US9657646B2 (en) | 2017-05-23 |
WO2014018137A3 (en) | 2014-04-17 |
JP2015514909A (ja) | 2015-05-21 |
CN104350237B (zh) | 2016-03-02 |
CA2870669A1 (en) | 2014-01-30 |
JP5856711B2 (ja) | 2016-02-10 |
EP2841712A2 (en) | 2015-03-04 |
US20150139791A1 (en) | 2015-05-21 |
WO2014018137A2 (en) | 2014-01-30 |
CN104350237A (zh) | 2015-02-11 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B06F | Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette] | ||
B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] |
Free format text: REFERENTE A 6A ANUIDADE. |
|
B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |
Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2510 DE 12-02-2019 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013. |