JP4820545B2 - 後方flade式エンジン - Google Patents
後方flade式エンジン Download PDFInfo
- Publication number
- JP4820545B2 JP4820545B2 JP2004336213A JP2004336213A JP4820545B2 JP 4820545 B2 JP4820545 B2 JP 4820545B2 JP 2004336213 A JP2004336213 A JP 2004336213A JP 2004336213 A JP2004336213 A JP 2004336213A JP 4820545 B2 JP4820545 B2 JP 4820545B2
- Authority
- JP
- Japan
- Prior art keywords
- flade
- fan
- engine
- turbine
- duct
- 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.)
- Expired - Fee Related
Links
- 239000012530 fluid Substances 0.000 claims description 28
- 238000004891 communication Methods 0.000 claims description 26
- 238000001816 cooling Methods 0.000 claims description 19
- 238000011144 upstream manufacturing Methods 0.000 claims description 7
- 230000003190 augmentative effect Effects 0.000 claims description 4
- 239000007789 gas Substances 0.000 description 24
- 238000013461 design Methods 0.000 description 12
- 239000000567 combustion gas Substances 0.000 description 6
- 239000000446 fuel Substances 0.000 description 6
- 230000008859 change Effects 0.000 description 5
- 230000004048 modification Effects 0.000 description 5
- 238000012986 modification Methods 0.000 description 5
- 230000008901 benefit Effects 0.000 description 4
- 238000012360 testing method Methods 0.000 description 4
- 238000002485 combustion reaction Methods 0.000 description 3
- 238000000605 extraction Methods 0.000 description 3
- 238000009434 installation Methods 0.000 description 3
- 239000002918 waste heat Substances 0.000 description 3
- 230000001627 detrimental effect Effects 0.000 description 2
- 230000002708 enhancing effect Effects 0.000 description 2
- 238000011084 recovery Methods 0.000 description 2
- 230000007704 transition Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000008602 contraction Effects 0.000 description 1
- 238000012942 design verification Methods 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000007246 mechanism Effects 0.000 description 1
- 238000005086 pumping Methods 0.000 description 1
- 239000007921 spray Substances 0.000 description 1
- 239000003381 stabilizer Substances 0.000 description 1
Images
Classifications
-
- 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
- F02K3/077—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 the plant being of the multiple flow type, i.e. having three or more flows
-
- 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
- F02K1/38—Introducing air inside the jet
- F02K1/386—Introducing air inside the jet mixing devices in the jet pipe, e.g. for mixing primary and secondary flow
-
- 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
- F02K3/065—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 and aft fans
-
- 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
- F05D2220/32—Application in turbines in gas turbines
- F05D2220/327—Application in turbines in gas turbines to drive shrouded, high solidity propeller
-
- 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
- F05D2250/00—Geometry
- F05D2250/60—Structure; Surface texture
- F05D2250/61—Structure; Surface texture corrugated
- F05D2250/611—Structure; Surface texture corrugated undulated
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)
- Control Of Turbines (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US10/719,884 | 2003-11-21 | ||
| US10/719,884 US7216475B2 (en) | 2003-11-21 | 2003-11-21 | Aft FLADE engine |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2005155621A JP2005155621A (ja) | 2005-06-16 |
| JP2005155621A5 JP2005155621A5 (enExample) | 2008-01-17 |
| JP4820545B2 true JP4820545B2 (ja) | 2011-11-24 |
Family
ID=34435816
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2004336213A Expired - Fee Related JP4820545B2 (ja) | 2003-11-21 | 2004-11-19 | 後方flade式エンジン |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US7216475B2 (enExample) |
| EP (1) | EP1533510B1 (enExample) |
| JP (1) | JP4820545B2 (enExample) |
| CN (1) | CN100404839C (enExample) |
Families Citing this family (123)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7032387B2 (en) * | 2004-01-20 | 2006-04-25 | Pratt & Whitney Canada Corp. | Axisymmetric flap on gas turbine exhaust centerbody |
| FR2866070B1 (fr) * | 2004-02-05 | 2008-12-05 | Snecma Moteurs | Turboreacteur a fort taux de dilution |
| FR2878287B1 (fr) * | 2004-11-25 | 2009-05-22 | Snecma Moteurs Sa | Turboreacteur double corps double flux avec generateur de courant electrique arriere |
| US7509797B2 (en) * | 2005-04-29 | 2009-03-31 | General Electric Company | Thrust vectoring missile turbojet |
| US7448199B2 (en) * | 2005-04-29 | 2008-11-11 | General Electric Company | Self powdered missile turbojet |
| US7475545B2 (en) * | 2005-04-29 | 2009-01-13 | General Electric Company | Fladed supersonic missile turbojet |
| US7424805B2 (en) * | 2005-04-29 | 2008-09-16 | General Electric Company | Supersonic missile turbojet engine |
| US7464536B2 (en) * | 2005-07-07 | 2008-12-16 | General Electric Company | Methods and apparatus for assembling gas turbine engines |
| WO2007037725A1 (en) * | 2005-09-27 | 2007-04-05 | Volvo Aero Corporation | An arrangement for propelling an aircraft, aircraft and outlet nozzle for a jet engine |
| FR2891248B1 (fr) * | 2005-09-28 | 2009-05-01 | Airbus France Sas | Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un mat d'accrochage d'un tel moteur |
| US7614210B2 (en) * | 2006-02-13 | 2009-11-10 | General Electric Company | Double bypass turbofan |
| US7631484B2 (en) * | 2006-03-13 | 2009-12-15 | Rollin George Giffin | High pressure ratio aft fan |
| FR2902830B1 (fr) * | 2006-06-27 | 2008-08-08 | Airbus France Sas | Turboreacteur pour aeronef |
| US7758303B1 (en) | 2006-07-31 | 2010-07-20 | General Electric Company | FLADE fan with different inner and outer airfoil stagger angles at a shroud therebetween |
| US7805925B2 (en) * | 2006-08-18 | 2010-10-05 | Pratt & Whitney Canada Corp. | Gas turbine engine exhaust duct ventilation |
| GB2443194B (en) | 2006-10-24 | 2008-09-10 | Rolls-Royce Plc | Gas turbine engine |
| US7514810B2 (en) * | 2006-12-15 | 2009-04-07 | General Electric Company | Electric power generation using power turbine aft of LPT |
| US7926290B2 (en) * | 2006-12-18 | 2011-04-19 | General Electric Company | Turbine engine with modulated flow fan and method of operation |
| US7877980B2 (en) * | 2006-12-28 | 2011-02-01 | General Electric Company | Convertible gas turbine engine |
| US7468561B2 (en) * | 2007-03-27 | 2008-12-23 | General Electric Company | Integrated electrical power extraction for aircraft engines |
| US8192141B1 (en) * | 2007-04-05 | 2012-06-05 | The United States Of America As Represented By The Secretary Of The Air Force | Dual compression rotor |
| FR2914943B1 (fr) * | 2007-04-13 | 2011-04-01 | Snecma | Aube de soufflante |
| GB2449095B (en) * | 2007-05-10 | 2009-05-27 | Rolls Royce Plc | Re-Pressurisation device |
| US8161728B2 (en) * | 2007-06-28 | 2012-04-24 | United Technologies Corp. | Gas turbines with multiple gas flow paths |
| US8708643B2 (en) * | 2007-08-14 | 2014-04-29 | General Electric Company | Counter-rotatable fan gas turbine engine with axial flow positive displacement worm gas generator |
| FR2920132B1 (fr) * | 2007-08-20 | 2009-09-18 | Aircelle Sa | Troncon arriere de nacelle d'aeronef et nacelle equipee d'un tel troncon arriere |
| FR2923270B1 (fr) * | 2007-11-06 | 2014-01-31 | Airbus France | Turbomoteur a tuyere de flux froid adaptee |
| US7969122B2 (en) * | 2007-11-14 | 2011-06-28 | Hamilton Sundstrand Corporation | Pole count changing generator |
| US8590286B2 (en) * | 2007-12-05 | 2013-11-26 | United Technologies Corp. | Gas turbine engine systems involving tip fans |
| US8739548B2 (en) * | 2007-12-20 | 2014-06-03 | United Technologies Corporation | Sliding ramp nozzle system for a gas turbine engine |
| US8127528B2 (en) * | 2008-02-26 | 2012-03-06 | United Technologies Corporation | Auxiliary propulsor for a variable cycle gas turbine engine |
| US8082727B2 (en) * | 2008-02-26 | 2011-12-27 | United Technologies Corporation | Rear propulsor for a variable cycle gas turbine engine |
| JP5092143B2 (ja) * | 2008-03-07 | 2012-12-05 | 独立行政法人 宇宙航空研究開発機構 | 高バイパス比ターボファンジェットエンジン |
| GB0809336D0 (en) * | 2008-05-23 | 2008-07-02 | Rolls Royce Plc | A gas turbine engine arrangement |
| US8128021B2 (en) | 2008-06-02 | 2012-03-06 | United Technologies Corporation | Engine mount system for a turbofan gas turbine engine |
| US20140174056A1 (en) | 2008-06-02 | 2014-06-26 | United Technologies Corporation | Gas turbine engine with low stage count low pressure turbine |
| US20100031669A1 (en) * | 2008-08-06 | 2010-02-11 | Cessna Aircraft Company | Free Turbine Generator For Aircraft |
| EP2177735A3 (en) * | 2008-10-20 | 2012-02-15 | Rolls-Royce North American Technologies, Inc. | Turbofan |
| ES2370308B1 (es) * | 2008-12-31 | 2012-10-22 | Futur Investment Partners, S.A. | Motor aeronáutico. |
| US8375695B2 (en) * | 2009-06-30 | 2013-02-19 | General Electric Company | Aircraft gas turbine engine counter-rotatable generator |
| US20110167791A1 (en) * | 2009-09-25 | 2011-07-14 | James Edward Johnson | Convertible fan engine |
| US20110167792A1 (en) * | 2009-09-25 | 2011-07-14 | James Edward Johnson | Adaptive engine |
| US20110179766A1 (en) * | 2009-10-27 | 2011-07-28 | Fly Steam, LLC | Heat recovery system |
| US8499544B2 (en) * | 2009-11-17 | 2013-08-06 | General Electric Company | Turbogenerator with cooling system |
| US8695324B2 (en) | 2009-11-20 | 2014-04-15 | General Electric Co. | Multistage tip fan |
| US9353684B2 (en) * | 2009-12-11 | 2016-05-31 | Northrop Grumman Systems Corporation | Aircraft engine airflow modulation apparatus and method for engine bay cooling and cycle flow matching |
| CN101737194B (zh) * | 2009-12-18 | 2013-06-05 | 北京航空航天大学 | 一种变循环发动机模式转换机构中的可调前涵道引射器 |
| US8063528B2 (en) * | 2009-12-18 | 2011-11-22 | General Electric Company | Counter-rotatable generator |
| CA2724611A1 (en) * | 2009-12-21 | 2011-06-21 | General Electric Company | Power extraction system |
| US20110146228A1 (en) * | 2009-12-21 | 2011-06-23 | John Lewis Baughman | Power extraction system |
| US20110146289A1 (en) * | 2009-12-21 | 2011-06-23 | John Lewis Baughman | Power extraction method |
| DE102010009477A1 (de) * | 2010-02-26 | 2011-09-01 | Rolls-Royce Deutschland Ltd & Co Kg | Fluggasturbinenantrieb |
| FR2966522B1 (fr) * | 2010-10-26 | 2015-04-24 | Snecma | Turbomachine a double soufflante et triple flux |
| US9016041B2 (en) * | 2010-11-30 | 2015-04-28 | General Electric Company | Variable-cycle gas turbine engine with front and aft FLADE stages |
| FR2972769B1 (fr) * | 2011-03-16 | 2015-07-03 | Snecma | Turbomachine a triple flux |
| FR2975135B1 (fr) * | 2011-05-12 | 2016-07-22 | Snecma | Cone arriere de turboreacteur tournant a micro-jets |
| US8789376B2 (en) * | 2011-05-27 | 2014-07-29 | General Electric Company | Flade duct turbine cooling and power and thermal management |
| US9523422B2 (en) | 2011-06-08 | 2016-12-20 | United Technologies Corporation | Flexible support structure for a geared architecture gas turbine engine |
| US9239012B2 (en) | 2011-06-08 | 2016-01-19 | United Technologies Corporation | Flexible support structure for a geared architecture gas turbine engine |
| US9631558B2 (en) | 2012-01-03 | 2017-04-25 | United Technologies Corporation | Geared architecture for high speed and small volume fan drive turbine |
| CA2839412A1 (en) * | 2011-06-14 | 2012-12-20 | Rolls-Royce North American Technologies, Inc. | Aircraft powerplant |
| WO2013077924A2 (en) * | 2011-09-08 | 2013-05-30 | Rolls-Royce North American Technologies Inc. | Gas turbine engine system and supersonic exhaust nozzle |
| US9777631B2 (en) | 2011-09-30 | 2017-10-03 | General Electric Company | Conformal inlet apparatus for a gas turbine engine |
| US9279388B2 (en) | 2011-11-01 | 2016-03-08 | United Technologies Corporation | Gas turbine engine with two-spool fan and variable vane turbine |
| US10287914B2 (en) | 2012-01-31 | 2019-05-14 | United Technologies Corporation | Gas turbine engine with high speed low pressure turbine section and bearing support features |
| US20130192256A1 (en) * | 2012-01-31 | 2013-08-01 | Gabriel L. Suciu | Geared turbofan engine with counter-rotating shafts |
| US10125693B2 (en) | 2012-04-02 | 2018-11-13 | United Technologies Corporation | Geared turbofan engine with power density range |
| US20150308351A1 (en) | 2012-05-31 | 2015-10-29 | United Technologies Corporation | Fundamental gear system architecture |
| US8756908B2 (en) | 2012-05-31 | 2014-06-24 | United Technologies Corporation | Fundamental gear system architecture |
| US8572943B1 (en) | 2012-05-31 | 2013-11-05 | United Technologies Corporation | Fundamental gear system architecture |
| US9140212B2 (en) | 2012-06-25 | 2015-09-22 | United Technologies Corporation | Gas turbine engine with reverse-flow core having a bypass flow splitter |
| EP2959146B1 (en) * | 2013-02-19 | 2018-04-04 | United Technologies Corporation | Turbofan engine including third flowpath exhaust nozzle |
| US9003638B2 (en) | 2013-03-11 | 2015-04-14 | Pratt & Whitney Canada Corp. | Method of assembling an electromechanical device in a gas-turbine engine |
| US8829702B1 (en) * | 2013-03-11 | 2014-09-09 | Pratt & Whitney Canada Corp | Gas turbine engine with internal electromechanical device |
| US9863366B2 (en) * | 2013-03-13 | 2018-01-09 | Rolls-Royce North American Technologies Inc. | Exhaust nozzle apparatus and method for multi stream aircraft engine |
| US9523329B2 (en) | 2013-03-15 | 2016-12-20 | United Technologies Corporation | Gas turbine engine with stream diverter |
| EP3008323B1 (en) | 2013-05-09 | 2021-11-10 | Raytheon Technologies Corporation | Turbofan engine front section |
| EP2994628A4 (en) | 2013-05-09 | 2017-01-18 | United Technologies Corporation | Turbofan engine front section |
| FR3008740B1 (fr) * | 2013-07-18 | 2017-11-24 | Snecma | Turbomachine comportant un melangeur a lobes entre un generateur de gaz et une turbine. |
| US9371776B2 (en) | 2013-08-20 | 2016-06-21 | Darren Levine | Dual flow air injection intraturbine engine and method of operating same |
| US10400709B2 (en) | 2013-09-20 | 2019-09-03 | United Technologies Corporation | Auxiliary device for three air flow path gas turbine engine |
| US9909529B2 (en) | 2013-09-20 | 2018-03-06 | United Technologies Corporation | Flow path routing within a gas turbine engine |
| US10371090B2 (en) | 2014-01-13 | 2019-08-06 | United Technologies Corporation | Variable area exhaust mixer for a gas turbine engine |
| US10030606B2 (en) | 2014-01-27 | 2018-07-24 | United Technologies Corporation | Variable exhaust mixer and cooler for a three-stream gas turbine engine |
| US9951721B2 (en) | 2014-10-21 | 2018-04-24 | United Technologies Corporation | Three-stream gas turbine engine architecture |
| US11236639B2 (en) * | 2015-02-10 | 2022-02-01 | Raytheon Technologies Corporation | Gas turbine engine and an airflow control system |
| EP3249205B1 (en) | 2015-05-27 | 2020-01-29 | IHI Corporation | Jet engine |
| US10443539B2 (en) | 2015-11-23 | 2019-10-15 | Rolls-Royce North American Technologies Inc. | Hybrid exhaust nozzle |
| US10677158B2 (en) * | 2015-12-29 | 2020-06-09 | General Electric Company | Method and system for in-line distributed propulsion |
| US10794281B2 (en) * | 2016-02-02 | 2020-10-06 | General Electric Company | Gas turbine engine having instrumented airflow path components |
| US10151217B2 (en) * | 2016-02-11 | 2018-12-11 | General Electric Company | Turbine frame cooling systems and methods of assembly for use in a gas turbine engine |
| FR3050485B1 (fr) * | 2016-04-26 | 2020-04-10 | Safran Aircraft Engines | Turbomachine a double flux |
| US20170314509A1 (en) * | 2016-04-27 | 2017-11-02 | General Electric Company | Turbofan assembly and method of assembling |
| US10563516B2 (en) | 2016-07-06 | 2020-02-18 | General Electric Company | Turbine engine and method of assembling |
| US10287024B2 (en) | 2016-08-04 | 2019-05-14 | United Technologies Corporation | Direct drive aft fan engine |
| US10352274B2 (en) | 2016-08-18 | 2019-07-16 | United Technologies Corporation | Direct drive aft fan engine |
| RU2644660C1 (ru) * | 2017-03-07 | 2018-02-13 | Акционерное общество "ОДК-Авиадвигатель" | Газотурбинный двигатель |
| RU2669420C1 (ru) * | 2017-04-12 | 2018-10-11 | Владимир Леонидович Письменный | Двухконтурный турбореактивный двигатель |
| RU2675167C1 (ru) * | 2017-10-30 | 2018-12-17 | Владимир Леонидович Письменный | Газотурбинная установка |
| FR3085435B1 (fr) * | 2018-09-05 | 2021-06-18 | Safran Aircraft Engines | Turbomachine a double flux |
| RU2728577C2 (ru) * | 2018-10-03 | 2020-07-31 | Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") | Турбореактивный двухконтурный двигатель с раздельным истечением потоков из сопел |
| FR3087823B1 (fr) * | 2018-10-26 | 2020-11-13 | Safran Aircraft Engines | Module de soufflante equipe d'une machine electrique pour une turbomachine d'aeronef |
| US12044194B2 (en) * | 2019-10-15 | 2024-07-23 | General Electric Company | Propulsion system architecture |
| CN112727635B (zh) * | 2020-12-31 | 2022-04-26 | 中国航空发动机研究院 | 一种双外涵发动机 |
| CN113323769A (zh) * | 2021-06-07 | 2021-08-31 | 北京航空航天大学 | 一种基于多涵道进气级间燃烧室的变循环发动机构型 |
| RU208402U1 (ru) * | 2021-08-03 | 2021-12-16 | Общество с ограниченной ответственностью "Оверхол-Про" | Турбонагреватель газа |
| US11492918B1 (en) | 2021-09-03 | 2022-11-08 | General Electric Company | Gas turbine engine with third stream |
| US20230117984A1 (en) * | 2021-10-14 | 2023-04-20 | General Electric Company | Heat engine with heat exchanger |
| CN113738530B (zh) * | 2021-10-15 | 2022-06-17 | 清华大学 | 带叶尖风扇的多涵道航空发动机机匣结构 |
| US12065989B2 (en) | 2022-04-11 | 2024-08-20 | General Electric Company | Gas turbine engine with third stream |
| US11834954B2 (en) | 2022-04-11 | 2023-12-05 | General Electric Company | Gas turbine engine with third stream |
| US12410763B2 (en) | 2022-08-02 | 2025-09-09 | General Electric Company | Gas turbine engine with third stream |
| US12031504B2 (en) | 2022-08-02 | 2024-07-09 | General Electric Company | Gas turbine engine with third stream |
| US12421917B2 (en) | 2022-08-02 | 2025-09-23 | General Electric Company | Gas turbine engine with third stream |
| US12486817B2 (en) | 2022-08-02 | 2025-12-02 | General Electric Company | Gas turbine engine with third stream |
| US12428992B2 (en) | 2022-11-01 | 2025-09-30 | General Electric Company | Gas turbine engine |
| US12392290B2 (en) | 2022-11-01 | 2025-08-19 | General Electric Company | Gas turbine engine |
| US12410753B2 (en) | 2022-11-01 | 2025-09-09 | General Electric Company | Gas turbine engine |
| US12196131B2 (en) | 2022-11-01 | 2025-01-14 | General Electric Company | Gas turbine engine |
| US12388322B2 (en) | 2023-03-24 | 2025-08-12 | Rolls-Royce North American Technologies, Inc. | Electric generator behind fan in turbine engine |
| GB2633358A (en) * | 2023-09-07 | 2025-03-12 | Arthur Davies Mervyn | Dual induction jet DIJ |
| CN117738814B (zh) * | 2024-02-21 | 2024-05-17 | 中国航发四川燃气涡轮研究院 | 带叶尖风扇及串联压气机的变流路宽速域发动机 |
| CN120061999A (zh) * | 2025-02-21 | 2025-05-30 | 哈尔滨工业大学 | 一种基于旋转机匣的大涵道比涡扇发动机动力系统及设计方法 |
Family Cites Families (29)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3282053A (en) * | 1966-11-01 | Ducted fan arrangement for aircraft | ||
| US2405919A (en) * | 1940-03-02 | 1946-08-13 | Power Jets Res & Dev Ltd | Fluid flow energy transformer |
| US3348379A (en) * | 1963-09-25 | 1967-10-24 | Rolls Royce | Turbojet engine with compressor bypass and aft fan |
| GB981857A (en) * | 1963-12-03 | 1965-01-27 | Rolls Royce | Gas turbine engine |
| GB1212875A (en) * | 1967-12-21 | 1970-11-18 | Rolls Royce | Aircraft |
| US3673802A (en) | 1970-06-18 | 1972-07-04 | Gen Electric | Fan engine with counter rotating geared core booster |
| GB1321657A (en) * | 1970-09-16 | 1973-06-27 | Secr Defence | Ducted fan gas turbine jet propulsion engine |
| GB1330904A (en) | 1971-04-19 | 1973-09-19 | Secr Defence | Gas turbine jet propulsion engines |
| US3938328A (en) * | 1971-11-08 | 1976-02-17 | The Boeing Company | Multicycle engine |
| US4055949A (en) * | 1973-05-08 | 1977-11-01 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation | Multiflow gas turbine power plant |
| US4043121A (en) | 1975-01-02 | 1977-08-23 | General Electric Company | Two-spool variable cycle engine |
| US4068471A (en) | 1975-06-16 | 1978-01-17 | General Electric Company | Variable cycle engine with split fan section |
| US4222235A (en) | 1977-07-25 | 1980-09-16 | General Electric Company | Variable cycle engine |
| US4232515A (en) | 1978-03-06 | 1980-11-11 | The Boeing Company | Supersonic cruise airplane and engine |
| US4463772A (en) | 1981-09-29 | 1984-08-07 | The Boeing Company | Flush inlet for supersonic aircraft |
| US4592201A (en) * | 1982-07-12 | 1986-06-03 | General Electric Company | Turbofan mixed flow exhaust system |
| GB2246171B (en) * | 1986-06-21 | 1992-04-08 | British Aerospace | Improvements in or related to gas turbine engines |
| US5070690A (en) * | 1989-04-26 | 1991-12-10 | General Electric Company | Means and method for reducing differential pressure loading in an augmented gas turbine engine |
| GB8924871D0 (en) * | 1989-11-03 | 1989-12-20 | Rolls Royce Plc | Tandem fan engine |
| CA2091473A1 (en) | 1992-04-20 | 1993-10-21 | Mark J. Wagner | Bypass injector valve for variable cycle aircraft engines |
| US5261227A (en) | 1992-11-24 | 1993-11-16 | General Electric Company | Variable specific thrust turbofan engine |
| US5388964A (en) | 1993-09-14 | 1995-02-14 | General Electric Company | Hybrid rotor blade |
| US5402638A (en) | 1993-10-04 | 1995-04-04 | General Electric Company | Spillage drag reducing flade engine |
| US5404713A (en) * | 1993-10-04 | 1995-04-11 | General Electric Company | Spillage drag and infrared reducing flade engine |
| US5809772A (en) | 1996-03-29 | 1998-09-22 | General Electric Company | Turbofan engine with a core driven supercharged bypass duct |
| US5806303A (en) | 1996-03-29 | 1998-09-15 | General Electric Company | Turbofan engine with a core driven supercharged bypass duct and fixed geometry nozzle |
| US5794432A (en) | 1996-08-27 | 1998-08-18 | Diversitech, Inc. | Variable pressure and variable air flow turbofan engines |
| US5931636A (en) | 1997-08-28 | 1999-08-03 | General Electric Company | Variable area turbine nozzle |
| US6732502B2 (en) * | 2002-03-01 | 2004-05-11 | General Electric Company | Counter rotating aircraft gas turbine engine with high overall pressure ratio compressor |
-
2003
- 2003-11-21 US US10/719,884 patent/US7216475B2/en active Active
-
2004
- 2004-11-17 EP EP04257144A patent/EP1533510B1/en not_active Expired - Lifetime
- 2004-11-19 JP JP2004336213A patent/JP4820545B2/ja not_active Expired - Fee Related
- 2004-11-22 CN CNB2004100950316A patent/CN100404839C/zh not_active Expired - Lifetime
Also Published As
| Publication number | Publication date |
|---|---|
| EP1533510B1 (en) | 2011-08-31 |
| EP1533510A3 (en) | 2009-02-18 |
| CN100404839C (zh) | 2008-07-23 |
| JP2005155621A (ja) | 2005-06-16 |
| US20050109012A1 (en) | 2005-05-26 |
| EP1533510A2 (en) | 2005-05-25 |
| CN1619129A (zh) | 2005-05-25 |
| US7216475B2 (en) | 2007-05-15 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP4820545B2 (ja) | 後方flade式エンジン | |
| JP4820619B2 (ja) | Flade式ガスタービンエンジンおよび航空機 | |
| JP4619089B2 (ja) | 固定ジオメトリ入口を備えたfladeガスタービンエンジン | |
| JP4856366B2 (ja) | 二重反転ファンを備えたfladeガスタービンエンジン | |
| JP2607051B2 (ja) | 航空機フレード・ガスタービンエンジン及び航空機フレード・ガスタービンエンジンを運転する方法 | |
| JP2686419B2 (ja) | 航空機フレード・ガスタービンエンジン及び航空機フレード・ガスタービンエンジンを運転する方法 | |
| JP4953924B2 (ja) | 内側及び外側翼形部間のシュラウドの位置において異なる内側及び外側翼形部食違い角を有するfladeファン | |
| JP5968329B2 (ja) | 一体型可変形状流量制限器および熱交換器 | |
| JP5220400B2 (ja) | ダクト燃焼式混成流ターボファン | |
| JP2007516376A (ja) | 航空機用エンジン装置 | |
| JP2011085141A (ja) | ガスタービンエンジン温度調節冷却流 | |
| JP4920228B2 (ja) | ガスタービンエンジンを組み立てるための方法及び装置 | |
| CN115788679B (zh) | 废热回收系统 | |
| US12037943B2 (en) | Waste heat recovery system | |
| CN118223957A (zh) | 涡轮风扇发动机的出口导向轮叶组件 | |
| CN118223958A (zh) | 涡轮风扇发动机的出口导向轮叶组件 | |
| CN121001929A (zh) | 具有第三流的燃气涡轮发动机 | |
| US12044172B2 (en) | Air guide for a gas turbine engine | |
| US12392287B2 (en) | Steam cooling turbine stator vane array | |
| CN119062447A (zh) | 燃气涡轮发动机 | |
| CN117588275A (zh) | 燃气涡轮发动机 |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| A521 | Written amendment |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20071116 |
|
| A621 | Written request for application examination |
Free format text: JAPANESE INTERMEDIATE CODE: A621 Effective date: 20071116 |
|
| A131 | Notification of reasons for refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A131 Effective date: 20100126 |
|
| A601 | Written request for extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A601 Effective date: 20100422 |
|
| RD02 | Notification of acceptance of power of attorney |
Free format text: JAPANESE INTERMEDIATE CODE: A7422 Effective date: 20100422 |
|
| RD04 | Notification of resignation of power of attorney |
Free format text: JAPANESE INTERMEDIATE CODE: A7424 Effective date: 20100422 |
|
| A602 | Written permission of extension of time |
Free format text: JAPANESE INTERMEDIATE CODE: A602 Effective date: 20100428 |
|
| A521 | Written amendment |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20100726 |
|
| A521 | Written amendment |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20100826 |
|
| A02 | Decision of refusal |
Free format text: JAPANESE INTERMEDIATE CODE: A02 Effective date: 20110125 |
|
| A521 | Written amendment |
Free format text: JAPANESE INTERMEDIATE CODE: A523 Effective date: 20110524 |
|
| A911 | Transfer of reconsideration by examiner before appeal (zenchi) |
Free format text: JAPANESE INTERMEDIATE CODE: A911 Effective date: 20110531 |
|
| TRDD | Decision of grant or rejection written | ||
| A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 Effective date: 20110809 |
|
| A01 | Written decision to grant a patent or to grant a registration (utility model) |
Free format text: JAPANESE INTERMEDIATE CODE: A01 |
|
| A61 | First payment of annual fees (during grant procedure) |
Free format text: JAPANESE INTERMEDIATE CODE: A61 Effective date: 20110905 |
|
| FPAY | Renewal fee payment (event date is renewal date of database) |
Free format text: PAYMENT UNTIL: 20140909 Year of fee payment: 3 |
|
| R150 | Certificate of patent or registration of utility model |
Free format text: JAPANESE INTERMEDIATE CODE: R150 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| R250 | Receipt of annual fees |
Free format text: JAPANESE INTERMEDIATE CODE: R250 |
|
| LAPS | Cancellation because of no payment of annual fees |