BR112014031175A2 - motor de turbina a gás e conduto de fluido. - Google Patents
motor de turbina a gás e conduto de fluido.Info
- Publication number
- BR112014031175A2 BR112014031175A2 BR112014031175A BR112014031175A BR112014031175A2 BR 112014031175 A2 BR112014031175 A2 BR 112014031175A2 BR 112014031175 A BR112014031175 A BR 112014031175A BR 112014031175 A BR112014031175 A BR 112014031175A BR 112014031175 A2 BR112014031175 A2 BR 112014031175A2
- Authority
- BR
- Brazil
- Prior art keywords
- gas turbine
- turbine engine
- fluid duct
- duct
- fluid
- 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
- F02C7/22—Fuel supply systems
- F02C7/222—Fuel flow conduits, e.g. manifolds
-
- 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
-
- 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
- F02C7/24—Heat or noise insulation
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
- Control Of Turbines (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201261660533P | 2012-06-15 | 2012-06-15 | |
PCT/US2013/045766 WO2013188723A1 (en) | 2012-06-15 | 2013-06-14 | Fluid conduit |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112014031175A2 true BR112014031175A2 (pt) | 2017-06-27 |
Family
ID=48699976
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112014031175A BR112014031175A2 (pt) | 2012-06-15 | 2013-06-14 | motor de turbina a gás e conduto de fluido. |
Country Status (7)
Country | Link |
---|---|
US (1) | US9784187B2 (pt) |
EP (1) | EP2877711A1 (pt) |
JP (1) | JP2015520356A (pt) |
CN (1) | CN104379879B (pt) |
BR (1) | BR112014031175A2 (pt) |
CA (1) | CA2875800C (pt) |
WO (1) | WO2013188723A1 (pt) |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2823952A1 (de) * | 2013-07-09 | 2015-01-14 | Siemens Aktiengesellschaft | Anpassungsverfahren und Herstellverfahren für mittels SLM gefertigte Bauteile |
US9995220B2 (en) * | 2013-12-20 | 2018-06-12 | Pratt & Whitney Canada Corp. | Fluid manifold for gas turbine engine and method for delivering fuel to a combustor using same |
US9857002B2 (en) | 2014-05-09 | 2018-01-02 | United Technologies Corporation | Fluid couplings and methods for additive manufacturing thereof |
DE102014214842A1 (de) | 2014-07-29 | 2016-02-04 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbine mit konzentrischer Kraftstoffleitung und Anschluss an Duplexbrennerkopf |
US9874351B2 (en) | 2015-04-14 | 2018-01-23 | General Electric Company | Thermally-coupled fuel manifold |
CN109415980B (zh) * | 2016-06-30 | 2021-10-22 | 通用电气公司 | 集成流体管道 |
US20190234311A1 (en) * | 2018-01-29 | 2019-08-01 | Pratt & Whitney Canada Corp. | Thermal insulation for fluid carrying components |
US10605171B2 (en) * | 2018-04-10 | 2020-03-31 | Delavan Inc. | Fuel nozzle manifold systems for turbomachines |
US11156162B2 (en) | 2018-05-23 | 2021-10-26 | General Electric Company | Fluid manifold damper for gas turbine engine |
US11060459B2 (en) * | 2018-07-10 | 2021-07-13 | Delavan Inc. | Internal manifold for multipoint injection |
US11506125B2 (en) | 2018-08-01 | 2022-11-22 | General Electric Company | Fluid manifold assembly for gas turbine engine |
US11255270B2 (en) * | 2018-12-18 | 2022-02-22 | Delavan Inc. | Heat shielding for internal fuel manifolds |
US11226100B2 (en) * | 2019-07-22 | 2022-01-18 | Delavan Inc. | Fuel manifolds |
US11187155B2 (en) * | 2019-07-22 | 2021-11-30 | Delavan Inc. | Sectional fuel manifolds |
FR3100571B1 (fr) * | 2019-09-05 | 2021-07-30 | Safran Aircraft Engines | Canalisation pour une turbomachine d’aéronef |
US11369985B2 (en) * | 2019-10-04 | 2022-06-28 | Delavan Inc | Fluid conduits with heat shielding |
Family Cites Families (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4735044A (en) | 1980-11-25 | 1988-04-05 | General Electric Company | Dual fuel path stem for a gas turbine engine |
US4467610A (en) * | 1981-04-17 | 1984-08-28 | General Electric Company | Gas turbine fuel system |
CA2056480C (en) * | 1991-01-18 | 2000-01-04 | Thomas Maclean | Gas turbine engine fuel manifold |
CA2072275A1 (en) | 1991-08-12 | 1993-02-13 | Phillip D. Napoli | Fuel delivery system for dual annular combustor |
DE4204530A1 (de) * | 1992-02-15 | 1993-08-19 | Asea Brown Boveri | Rohrsystem |
US5218824A (en) | 1992-06-25 | 1993-06-15 | Solar Turbines Incorporated | Low emission combustion nozzle for use with a gas turbine engine |
US5263314A (en) * | 1992-09-28 | 1993-11-23 | General Motors Corporation | Fuel leakage protection system for gas turbine engine |
US6321541B1 (en) | 1999-04-01 | 2001-11-27 | Parker-Hannifin Corporation | Multi-circuit multi-injection point atomizer |
US7028484B2 (en) * | 2002-08-30 | 2006-04-18 | Pratt & Whitney Canada Corp. | Nested channel ducts for nozzle construction and the like |
US6959535B2 (en) | 2003-01-31 | 2005-11-01 | General Electric Company | Differential pressure induced purging fuel injectors |
US7654088B2 (en) | 2004-02-27 | 2010-02-02 | Pratt & Whitney Canada Corp. | Dual conduit fuel manifold for gas turbine engine |
US6955040B1 (en) | 2004-03-31 | 2005-10-18 | General Electric Company | Controlled pressure fuel nozzle injector |
US7269939B2 (en) | 2004-11-24 | 2007-09-18 | General Electric Company | Method and apparatus for automatically actuating fuel trim valves in a gas |
US7536862B2 (en) | 2005-09-01 | 2009-05-26 | General Electric Company | Fuel nozzle for gas turbine engines |
US7607226B2 (en) * | 2006-03-03 | 2009-10-27 | Pratt & Whitney Canada Corp. | Internal fuel manifold with turned channel having a variable cross-sectional area |
US7942002B2 (en) | 2006-03-03 | 2011-05-17 | Pratt & Whitney Canada Corp. | Fuel conveying member with side-brazed sealing members |
US8001761B2 (en) | 2006-05-23 | 2011-08-23 | General Electric Company | Method and apparatus for actively controlling fuel flow to a mixer assembly of a gas turbine engine combustor |
US8096130B2 (en) * | 2006-07-20 | 2012-01-17 | Pratt & Whitney Canada Corp. | Fuel conveying member for a gas turbine engine |
US7703289B2 (en) | 2006-09-18 | 2010-04-27 | Pratt & Whitney Canada Corp. | Internal fuel manifold having temperature reduction feature |
US7716933B2 (en) * | 2006-10-04 | 2010-05-18 | Pratt & Whitney Canada Corp. | Multi-channel fuel manifold |
US8096131B2 (en) | 2007-11-14 | 2012-01-17 | Pratt & Whitney Canada Corp. | Fuel inlet with crescent shaped passage for gas turbine engines |
US20090255120A1 (en) | 2008-04-11 | 2009-10-15 | General Electric Company | Method of assembling a fuel nozzle |
WO2009148680A2 (en) | 2008-04-11 | 2009-12-10 | General Electric Company | Unitary conduit for transporting fluids and method of manufacturing |
US20090255118A1 (en) * | 2008-04-11 | 2009-10-15 | General Electric Company | Method of manufacturing mixers |
US8234873B2 (en) * | 2008-08-28 | 2012-08-07 | Woodward, Inc. | Multi passage fuel manifold and methods of construction |
US8079220B2 (en) * | 2008-08-28 | 2011-12-20 | Delavan Inc | Fuel distribution manifold system for gas turbine engines |
US9194297B2 (en) * | 2010-12-08 | 2015-11-24 | Parker-Hannifin Corporation | Multiple circuit fuel manifold |
US9958093B2 (en) | 2010-12-08 | 2018-05-01 | Parker-Hannifin Corporation | Flexible hose assembly with multiple flow passages |
GB201401581D0 (en) | 2014-01-30 | 2014-03-19 | Rolls Royce Plc | A fuel manifold and fuel injector arrangement |
-
2013
- 2013-06-14 CN CN201380031620.5A patent/CN104379879B/zh active Active
- 2013-06-14 JP JP2015517444A patent/JP2015520356A/ja active Pending
- 2013-06-14 US US14/407,400 patent/US9784187B2/en active Active
- 2013-06-14 BR BR112014031175A patent/BR112014031175A2/pt not_active IP Right Cessation
- 2013-06-14 EP EP13732040.4A patent/EP2877711A1/en not_active Withdrawn
- 2013-06-14 WO PCT/US2013/045766 patent/WO2013188723A1/en active Application Filing
- 2013-06-14 CA CA2875800A patent/CA2875800C/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
EP2877711A1 (en) | 2015-06-03 |
US20150121883A1 (en) | 2015-05-07 |
CN104379879A (zh) | 2015-02-25 |
CA2875800A1 (en) | 2013-12-19 |
CN104379879B (zh) | 2016-08-24 |
WO2013188723A1 (en) | 2013-12-19 |
CA2875800C (en) | 2017-03-28 |
JP2015520356A (ja) | 2015-07-16 |
US9784187B2 (en) | 2017-10-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B06F | Objections, documents and/or translations needed after an examination request according art. 34 industrial property law | ||
B08F | Application fees: dismissal - article 86 of industrial property law |
Free format text: REFERENTE A 6A ANUIDADE. |
|
B08K | Lapse as no evidence of payment of the annual fee has been furnished to inpi (acc. art. 87) |
Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2518 DE 09-04-2019 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. |