CA2853694C - Moteur de turbine a gaz dote d'une architecture a engrenages - Google Patents
Moteur de turbine a gaz dote d'une architecture a engrenages Download PDFInfo
- Publication number
- CA2853694C CA2853694C CA2853694A CA2853694A CA2853694C CA 2853694 C CA2853694 C CA 2853694C CA 2853694 A CA2853694 A CA 2853694A CA 2853694 A CA2853694 A CA 2853694A CA 2853694 C CA2853694 C CA 2853694C
- Authority
- CA
- Canada
- Prior art keywords
- fan
- engine
- recited
- nacelle
- core
- 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
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- 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
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
- F01D17/16—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes
- F01D17/162—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes for axial flow, i.e. the vanes turning around axes which are essentially perpendicular to the rotor centre line
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/40—Casings; Connections of working fluid
- F04D29/52—Casings; Connections of working fluid for axial pumps
- F04D29/54—Fluid-guiding means, e.g. diffusers
- F04D29/56—Fluid-guiding means, e.g. diffusers adjustable
- F04D29/563—Fluid-guiding means, e.g. diffusers adjustable specially adapted for elastic fluid pumps
-
- 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
- F01D17/00—Regulating or controlling by varying flow
- F01D17/10—Final actuators
- F01D17/12—Final actuators arranged in stator parts
- F01D17/14—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits
-
- 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
- F02K1/06—Varying effective area of jet pipe or nozzle
-
- 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Turbines (AREA)
Abstract
La présente invention se rapporte, selon un aspect donné à titre d'exemple, à un moteur à turbine à gaz qui comprend une nacelle centrale définie autour d'un axe central de moteur, une nacelle de ventilateur montée au moins partiellement autour de la nacelle centrale pour définir un trajet d'écoulement de dérivation de ventilateur pour un flux d'air de dérivation de ventilateur, une buse de ventilateur à zone variable qui est axialement mobile par rapport à la nacelle de ventilateur afin de faire varier une zone de sortie de buse de ventilateur et de régler le rapport de pression du flux d'air de dérivation de ventilateur pendant le fonctionnement du moteur, et un système d'engrenages entraîné par un moteur central agencé dans la nacelle centrale afin d'entraîner un ventilateur agencé dans la nacelle de ventilateur, le système d'engrenages définissant un rapport de démultiplication supérieur ou égal à 2,3.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/346,100 | 2012-01-09 | ||
US13/346,100 US20120222398A1 (en) | 2007-07-27 | 2012-01-09 | Gas turbine engine with geared architecture |
PCT/US2013/020040 WO2013106223A1 (fr) | 2012-01-09 | 2013-01-03 | Moteur de turbine à gaz doté d'une architecture à engrenages |
Publications (2)
Publication Number | Publication Date |
---|---|
CA2853694A1 CA2853694A1 (fr) | 2013-07-18 |
CA2853694C true CA2853694C (fr) | 2016-03-22 |
Family
ID=48781820
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA2853694A Active CA2853694C (fr) | 2012-01-09 | 2013-01-03 | Moteur de turbine a gaz dote d'une architecture a engrenages |
Country Status (8)
Country | Link |
---|---|
EP (1) | EP2802745A4 (fr) |
JP (2) | JP2015503705A (fr) |
CN (1) | CN104040117A (fr) |
BR (1) | BR112014016602B1 (fr) |
CA (1) | CA2853694C (fr) |
RU (1) | RU2647558C2 (fr) |
SG (1) | SG11201402663XA (fr) |
WO (1) | WO2013106223A1 (fr) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA2862597C (fr) * | 2013-10-03 | 2018-12-11 | Karl L. Hasel | Architecture de turbine a gaz a engrenages pour une efficacite amelioree |
EP3048266A1 (fr) * | 2015-01-22 | 2016-07-27 | United Technologies Corporation | Moteur à turbine à gaz à faible rapport de pression de soufflante |
CN106286010B (zh) * | 2015-06-26 | 2018-10-26 | 中航空天发动机研究院有限公司 | 一种反向安装核心机的齿轮传动涡扇发动机 |
US9821917B2 (en) * | 2015-09-21 | 2017-11-21 | General Electric Company | Aft engine for an aircraft |
US10677264B2 (en) | 2016-10-14 | 2020-06-09 | General Electric Company | Supersonic single-stage turbofan engine |
US11421627B2 (en) | 2017-02-22 | 2022-08-23 | General Electric Company | Aircraft and direct drive engine under wing installation |
GB201719539D0 (en) * | 2017-11-24 | 2018-01-10 | Rolls Royce Plc | Gas Turbine Engine |
GB201811281D0 (en) * | 2018-07-10 | 2018-08-29 | Rolls Royce Plc | A geared turbofan bas turbine engine mounting arrangement |
GB201812553D0 (en) * | 2018-08-01 | 2018-09-12 | Rolls Royce Plc | Gas turbine engine |
GB201820930D0 (en) * | 2018-12-21 | 2019-02-06 | Rolls Royce Plc | Turbine engine |
GB201906168D0 (en) * | 2019-05-02 | 2019-06-19 | Rolls Royce Plc | Gas turbine engine with fan outlet guide vanes |
IT202000000652A1 (it) | 2020-01-15 | 2021-07-15 | Ge Avio Srl | Turbomacchina e gruppo ingranaggi |
Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3747343A (en) * | 1972-02-10 | 1973-07-24 | United Aircraft Corp | Low noise prop-fan |
US5259187A (en) * | 1993-02-05 | 1993-11-09 | General Electric Company | Method of operating an aircraft bypass turbofan engine having variable fan outlet guide vanes |
JPH09317557A (ja) * | 1996-05-30 | 1997-12-09 | Ishikawajima Harima Heavy Ind Co Ltd | ターボファンエンジン |
US5794432A (en) * | 1996-08-27 | 1998-08-18 | Diversitech, Inc. | Variable pressure and variable air flow turbofan engines |
US6732502B2 (en) * | 2002-03-01 | 2004-05-11 | General Electric Company | Counter rotating aircraft gas turbine engine with high overall pressure ratio compressor |
US6775990B2 (en) * | 2002-10-17 | 2004-08-17 | Mark Douglas Swinford | Methods and apparatus for regulating gas turbine engine fluid flow |
FR2866387B1 (fr) * | 2004-02-12 | 2008-03-14 | Snecma Moteurs | Adaptation aerodynamique de la soufflante arriere d'un turboreacteur double soufflante |
RU2315887C2 (ru) * | 2005-12-23 | 2008-01-27 | Открытое акционерное общество "Авиадвигатель" | Турбореактивный двигатель сверхвысокой степени двухконтурности |
US20100303608A1 (en) * | 2006-09-28 | 2010-12-02 | Mitsubishi Heavy Industries, Ltd. | Two-shaft gas turbine |
WO2008045074A1 (fr) * | 2006-10-12 | 2008-04-17 | United Technologies Corporation | Turboréacteur à double flux présentant une surface de sortie de tuyère de dilution variable et procédé permettant de le faire fonctionner |
EP2074312B1 (fr) * | 2006-10-12 | 2017-12-13 | United Technologies Corporation | Tuyère à section variable pour nacelle de soufflante de moteur à turbine à gaz équipée d' un système d'actionnement coulissant |
WO2008045058A1 (fr) * | 2006-10-12 | 2008-04-17 | United Technologies Corporation | Gestion de la ligne de fonctionnement d'un compresseur basse pression dans un moteur de turboréacteur à double flux |
WO2008045091A1 (fr) * | 2006-10-12 | 2008-04-17 | United Technologies Corporation | Buse à section variable d'un ventilateur de turbine à gaz équipée d'un système à pièces rapportées pivotantes |
US7721549B2 (en) * | 2007-02-08 | 2010-05-25 | United Technologies Corporation | Fan variable area nozzle for a gas turbine engine fan nacelle with cam drive ring actuation system |
US8127529B2 (en) * | 2007-03-29 | 2012-03-06 | United Technologies Corporation | Variable area fan nozzle and thrust reverser |
US20080310956A1 (en) * | 2007-06-13 | 2008-12-18 | Jain Ashok K | Variable geometry gas turbine engine nacelle assembly with nanoelectromechanical system |
US8347633B2 (en) | 2007-07-27 | 2013-01-08 | United Technologies Corporation | Gas turbine engine with variable geometry fan exit guide vane system |
US8074440B2 (en) * | 2007-08-23 | 2011-12-13 | United Technologies Corporation | Gas turbine engine with axial movable fan variable area nozzle |
US20110120079A1 (en) * | 2009-11-24 | 2011-05-26 | Schwark Jr Fred W | Variable area fan nozzle stiffeners and placement |
-
2013
- 2013-01-03 SG SG11201402663XA patent/SG11201402663XA/en unknown
- 2013-01-03 BR BR112014016602-1A patent/BR112014016602B1/pt active IP Right Grant
- 2013-01-03 WO PCT/US2013/020040 patent/WO2013106223A1/fr active Application Filing
- 2013-01-03 EP EP13735909.7A patent/EP2802745A4/fr not_active Withdrawn
- 2013-01-03 JP JP2014551302A patent/JP2015503705A/ja active Pending
- 2013-01-03 CA CA2853694A patent/CA2853694C/fr active Active
- 2013-01-03 RU RU2014130443A patent/RU2647558C2/ru active
- 2013-01-03 CN CN201380005057.4A patent/CN104040117A/zh active Pending
-
2016
- 2016-09-12 JP JP2016177200A patent/JP2017015095A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
RU2014130443A (ru) | 2016-02-27 |
EP2802745A4 (fr) | 2015-10-21 |
CN104040117A (zh) | 2014-09-10 |
SG11201402663XA (en) | 2014-09-26 |
BR112014016602B1 (pt) | 2022-03-29 |
WO2013106223A1 (fr) | 2013-07-18 |
RU2647558C2 (ru) | 2018-03-19 |
EP2802745A1 (fr) | 2014-11-19 |
JP2015503705A (ja) | 2015-02-02 |
CA2853694A1 (fr) | 2013-07-18 |
BR112014016602A8 (pt) | 2017-07-04 |
JP2017015095A (ja) | 2017-01-19 |
BR112014016602A2 (pt) | 2017-06-13 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
EEER | Examination request |
Effective date: 20140425 |