JP5512111B2 - ファン内に発電機を配置したターボジェット - Google Patents
ファン内に発電機を配置したターボジェット Download PDFInfo
- Publication number
- JP5512111B2 JP5512111B2 JP2008260354A JP2008260354A JP5512111B2 JP 5512111 B2 JP5512111 B2 JP 5512111B2 JP 2008260354 A JP2008260354 A JP 2008260354A JP 2008260354 A JP2008260354 A JP 2008260354A JP 5512111 B2 JP5512111 B2 JP 5512111B2
- Authority
- JP
- Japan
- Prior art keywords
- generator
- fan
- turbojet
- high pressure
- pressure spool
- 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
- 238000004804 winding Methods 0.000 claims description 21
- 239000007858 starting material Substances 0.000 claims description 5
- 239000000853 adhesive Substances 0.000 claims description 2
- 230000001070 adhesive effect Effects 0.000 claims description 2
- 230000005611 electricity Effects 0.000 description 12
- 238000001816 cooling Methods 0.000 description 4
- 239000000284 extract Substances 0.000 description 3
- 238000002485 combustion reaction Methods 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 1
- KPLQYGBQNPPQGA-UHFFFAOYSA-N cobalt samarium Chemical compound [Co].[Sm] KPLQYGBQNPPQGA-UHFFFAOYSA-N 0.000 description 1
- 229910052802 copper Inorganic materials 0.000 description 1
- 239000010949 copper Substances 0.000 description 1
- 230000009977 dual effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000005086 pumping Methods 0.000 description 1
- 229910000938 samarium–cobalt magnet Inorganic materials 0.000 description 1
Images
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
- F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
- F01D15/10—Adaptations for driving, or combinations with, electric generators
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- 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
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K21/00—Synchronous motors having permanent magnets; Synchronous generators having permanent magnets
- H02K21/12—Synchronous motors having permanent magnets; Synchronous generators having permanent magnets with stationary armatures and rotating magnets
- H02K21/14—Synchronous motors having permanent magnets; Synchronous generators having permanent magnets with stationary armatures and rotating magnets with magnets rotating within the armatures
-
- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02K—DYNAMO-ELECTRIC MACHINES
- H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
- H02K7/18—Structural association of electric generators with mechanical driving motors, e.g. with turbines
- H02K7/1807—Rotary generators
- H02K7/1823—Rotary generators structurally associated with turbines or similar engines
-
- 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
- F05D2220/70—Application in combination with
- F05D2220/76—Application in combination with an electrical generator
-
- 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
- F05D2220/70—Application in combination with
- F05D2220/76—Application in combination with an electrical generator
- F05D2220/764—Application in combination with an electrical generator of the alternating current (A.C.) type
-
- 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
- F05D2220/70—Application in combination with
- F05D2220/76—Application in combination with an electrical generator
- F05D2220/766—Application in combination with an electrical generator via a direct connection, i.e. a gearless transmission
-
- 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
- F05D2220/70—Application in combination with
- F05D2220/76—Application in combination with an electrical generator
- F05D2220/768—Application in combination with an electrical generator equipped with permanent magnets
Description
12 エンジンナセル
14 ファンケーシング
20 低圧スプール
22 低圧タービン
24 低圧コンプレッサ
30 高圧スプール
32 高圧タービン
34 高圧コンプレッサ
40 ファン
42 ファンブレード
60 発電機
62 ロータ
64 ステータ
66 巻線
68 永久磁石
70 電気ハーネス
72 AC/DCコンバータ
80 スクープ
82 冷却管
Claims (5)
- ナセル(12)と、高圧スプール(30)と、ナセルの一部を形成する固定ケーシング内に配設されたファン(40)を駆動する低圧スプール(20)と、ファン(40)内に配置され、そこから動力を取り出す、ファン内に組み込まれたロータを含む発電機(60)とを備えるターボジェットであって、発電機が、ファンケーシング(14)内に組み込まれたステータ(64)も含み、ロータが、ファンブレード(42)に固定された永久磁石(68)を備え、ターボジェットが、ステータ(64)を冷却するために、ファンケーシング(14)内に配置されたスクープ(80)をさらに含むことを特徴とする、ターボジェット。
- 前記磁石(68)が接着剤によって固定されていることを特徴とする、請求項1に記載のターボジェット。
- それぞれ高圧スプール(30)から動力を取り出し、または高圧スプール(30)に動力を供給する別の発電機および/または始動機をさらに含むこと特徴とする、請求項1または2に記載のターボジェット。
- ステータ(64)が、正に3つの巻線(66)を有することを特徴とする、請求項1から3のいずれか一項に記載のターボジェット。
- 前記発電機(60)が、AC/DCコンバータ(72)をさらに含むことを特徴とする、請求項1から4のいずれか一項に記載のターボジェット。
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0758130A FR2921978B1 (fr) | 2007-10-08 | 2007-10-08 | Turboreacteur a generateur electrique agence dans la soufflante |
FR0758130 | 2007-10-08 |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2009092068A JP2009092068A (ja) | 2009-04-30 |
JP5512111B2 true JP5512111B2 (ja) | 2014-06-04 |
Family
ID=39427658
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2008260354A Active JP5512111B2 (ja) | 2007-10-08 | 2008-10-07 | ファン内に発電機を配置したターボジェット |
Country Status (6)
Country | Link |
---|---|
US (1) | US7952244B2 (ja) |
EP (1) | EP2048329B1 (ja) |
JP (1) | JP5512111B2 (ja) |
CA (1) | CA2640048C (ja) |
FR (1) | FR2921978B1 (ja) |
RU (1) | RU2490497C2 (ja) |
Families Citing this family (43)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8146369B2 (en) * | 2007-11-06 | 2012-04-03 | Borealis Technical Limited | Integrated direct drive starter/generator for turbines |
US9143023B1 (en) * | 2010-05-17 | 2015-09-22 | Richard Christopher Uskert | Electromagnetic propulsive motor |
US9051881B2 (en) | 2010-12-28 | 2015-06-09 | Rolls-Royce Corporation | Electrical power generation and windmill starting for turbine engine and aircraft |
DE102011075097A1 (de) * | 2011-05-02 | 2012-11-08 | Krones Aktiengesellschaft | Vorrichtung zum Bewegen eines Fluids |
US9540998B2 (en) | 2011-05-27 | 2017-01-10 | Daniel K. Schlak | Integral gas turbine, flywheel, generator, and method for hybrid operation thereof |
DE102011082442A1 (de) * | 2011-09-09 | 2013-03-14 | Deere & Company | Wechselstromgenerator für ein Kraftfahrzeug |
US9194330B2 (en) * | 2012-07-31 | 2015-11-24 | United Technologies Corporation | Retrofitable auxiliary inlet scoop |
FR2994707B1 (fr) * | 2012-08-21 | 2018-04-06 | Snecma | Turbomachine hybride a helices contrarotatives |
US9038399B2 (en) | 2012-09-04 | 2015-05-26 | Pratt & Whitney Canada Corp. | Systems and methods for driving an oil cooling fan of a gas turbine engine |
EP2964904B1 (en) | 2013-03-03 | 2020-10-14 | Rolls-Royce North American Technologies, Inc. | Gas turbine engine |
US9879601B2 (en) | 2013-03-05 | 2018-01-30 | Rolls-Royce North American Technologies Inc. | Gas turbine engine component arrangement |
WO2014163698A1 (en) | 2013-03-07 | 2014-10-09 | Vandervaart Peter L | Cooled gas turbine engine component |
US9586690B2 (en) | 2013-03-14 | 2017-03-07 | Rolls-Royce Corporation | Hybrid turbo electric aero-propulsion system control |
EP3004564A4 (en) * | 2013-06-07 | 2016-11-23 | Ge Aviat Systems Llc | TURBO FAN MOTOR WITH GENERATOR |
US9494044B1 (en) * | 2014-04-02 | 2016-11-15 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Turbo-electric compressor/generator using Halbach arrays |
US10000293B2 (en) | 2015-01-23 | 2018-06-19 | General Electric Company | Gas-electric propulsion system for an aircraft |
DE102016202741A1 (de) * | 2016-02-23 | 2017-08-24 | Siemens Aktiengesellschaft | Rotor und elektrische Maschine |
US9764848B1 (en) | 2016-03-07 | 2017-09-19 | General Electric Company | Propulsion system for an aircraft |
DE102016207517A1 (de) | 2016-05-02 | 2017-11-02 | Siemens Aktiengesellschaft | Antriebssystem für Luftfahrzeug mit elektrischem Generator |
US10093428B2 (en) | 2016-08-22 | 2018-10-09 | General Electric Company | Electric propulsion system |
US10308366B2 (en) | 2016-08-22 | 2019-06-04 | General Electric Company | Embedded electric machine |
US10071811B2 (en) | 2016-08-22 | 2018-09-11 | General Electric Company | Embedded electric machine |
US10487839B2 (en) | 2016-08-22 | 2019-11-26 | General Electric Company | Embedded electric machine |
FR3062255B1 (fr) * | 2017-01-26 | 2019-06-21 | Commissariat A L'energie Atomique Et Aux Energies Alternatives | Convertisseur electrostatique |
US10822103B2 (en) * | 2017-02-10 | 2020-11-03 | General Electric Company | Propulsor assembly for an aircraft |
US10793281B2 (en) | 2017-02-10 | 2020-10-06 | General Electric Company | Propulsion system for an aircraft |
US11149578B2 (en) | 2017-02-10 | 2021-10-19 | General Electric Company | Propulsion system for an aircraft |
US10762726B2 (en) | 2017-06-13 | 2020-09-01 | General Electric Company | Hybrid-electric propulsion system for an aircraft |
CN107313876B (zh) * | 2017-07-04 | 2019-06-04 | 南京航空航天大学 | 一种用于航空涡扇发动机的磁悬浮外涵风扇 |
WO2019018832A2 (en) * | 2017-07-20 | 2019-01-24 | Zornes David Allen | PRODUCTION OF AERODYNAMIC END PITCH PROFILE IN A ROTARY VESSEL AIRCRAFT |
US11261787B2 (en) * | 2018-06-22 | 2022-03-01 | General Electric Company | Aircraft anti-icing system |
US10773812B2 (en) * | 2018-08-17 | 2020-09-15 | Raytheon Technologies Corporation | Hybrid electric aircraft battery charging |
US11156128B2 (en) | 2018-08-22 | 2021-10-26 | General Electric Company | Embedded electric machine |
US11097849B2 (en) | 2018-09-10 | 2021-08-24 | General Electric Company | Aircraft having an aft engine |
FR3087824B1 (fr) | 2018-10-26 | 2021-10-15 | Safran Aircraft Engines | Module electrique de soufflante d'aeronef comportant des aubes a fixation amelioree |
FR3087819B1 (fr) * | 2018-10-26 | 2020-11-13 | Safran Aircraft Engines | Turbomachine d'aeronef equipee d'une machine electrique |
FR3087821B1 (fr) | 2018-10-26 | 2021-12-03 | Safran Aircraft Engines | Module electrique de soufflante d'aeronef comportant des aubes a fixation perfectionnee |
FR3087822B1 (fr) | 2018-10-26 | 2020-11-06 | Safran Aircraft Engines | Turbomachine a machine electrique comportant un anneau de rotor accole a la soufflante |
US10807730B2 (en) * | 2018-12-21 | 2020-10-20 | General Electric Company | Motor driven propulsor of an aircraft |
GB201900378D0 (en) | 2019-01-11 | 2019-02-27 | Rolls Royce Plc | Electric machine |
US11162379B2 (en) * | 2019-03-15 | 2021-11-02 | Hamilton Sundstrand Corporation | Temperature control device for tail cone mounted generator |
FR3098846A1 (fr) | 2019-07-15 | 2021-01-22 | Airbus Operations | Groupe propulseur configuré pour déconnecter le rotor et le stator d’un moteur électrique |
US11692513B2 (en) * | 2021-11-01 | 2023-07-04 | Yuriy Radzikh | Electric jet engine |
Family Cites Families (28)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2853638A (en) * | 1957-01-11 | 1958-09-23 | Gen Motors Corp | Inductor generator |
GB1174969A (en) * | 1967-10-20 | 1969-12-17 | Rolls Royce | Gas Turbine Engine Provided with an Alternator |
GB1291943A (en) * | 1970-02-11 | 1972-10-04 | Secr Defence | Improvements in or relating to ducted fans |
US3796511A (en) * | 1972-06-15 | 1974-03-12 | Frigidraulic Inc | Blower |
US4057270A (en) * | 1975-04-03 | 1977-11-08 | Barry Alan Lebost | Fluid turbine |
CH606801A5 (ja) * | 1975-12-02 | 1978-11-15 | Escher Wyss Ag | |
US4367413A (en) * | 1980-06-02 | 1983-01-04 | Ramon Nair | Combined turbine and generator |
GB2185719B (en) * | 1986-01-25 | 1989-11-01 | Rolls Royce | Fluid flow reversing apparatus |
US5223759A (en) * | 1987-12-24 | 1993-06-29 | Seiko Epson Corporation | DC brushless motor with solid rotor having permanent magnet |
US5220231A (en) * | 1990-08-23 | 1993-06-15 | Westinghouse Electric Corp. | Integral motor propulsor unit for water vehicles |
US5607329A (en) * | 1995-12-21 | 1997-03-04 | The United States Of America As Represented By The Secretary Of The Navy | Integrated motor/marine propulsor with permanent magnet blades |
US6249071B1 (en) * | 1998-10-14 | 2001-06-19 | Advanced Rotary Systems Llc | Rotor drive motor with u-shaped stator cores |
JP2001107751A (ja) * | 1999-10-05 | 2001-04-17 | Honda Motor Co Ltd | 航空機用ガスタービン・エンジンの制御装置 |
GB2360752A (en) * | 2000-04-01 | 2001-10-03 | Glyn Jones | Helicopter without tail rotor |
GB2409936B (en) * | 2001-02-09 | 2005-09-14 | Rolls Royce Plc | Gas turbine with electrical machine |
DE10357503A1 (de) * | 2003-12-09 | 2005-07-07 | BSH Bosch und Siemens Hausgeräte GmbH | Ansteuerung eines Gleichstrommotors |
DE102004004945A1 (de) * | 2004-01-31 | 2005-08-18 | Mtu Aero Engines Gmbh | Gasturbine, insbesondere Flugtriebwerk |
GB0410778D0 (en) * | 2004-05-13 | 2004-06-16 | Rolls Royce Plc | Blade arrangement |
US7154191B2 (en) * | 2004-06-30 | 2006-12-26 | General Electric Company | Electrical machine with double-sided rotor |
US7443066B2 (en) * | 2005-07-29 | 2008-10-28 | General Electric Company | Methods and apparatus for cooling wind turbine generators |
US20070029803A1 (en) * | 2005-08-04 | 2007-02-08 | Randall Edward R | Machine for transferring power and producing electricity in a jet engine |
CN100514793C (zh) * | 2005-09-23 | 2009-07-15 | 富准精密工业(深圳)有限公司 | 马达及采用该马达的风扇 |
DE102005046208A1 (de) | 2005-09-28 | 2007-03-29 | Mtu Aero Engines Gmbh | Strahltriebwerk |
US7802757B2 (en) * | 2005-11-09 | 2010-09-28 | Pratt & Whitney Canada Corp. | Method and system for taxiing an aircraft |
US20070265761A1 (en) * | 2006-05-11 | 2007-11-15 | Dooley Kevin A | Electric power generation system and method |
US7603864B2 (en) * | 2006-11-29 | 2009-10-20 | General Electric Company | Blade tip electric machine |
US7854582B2 (en) * | 2007-05-08 | 2010-12-21 | Pratt & Whitney Canada Corp. | Operation of an aircraft engine after emergency shutdown |
US8282337B2 (en) * | 2007-12-28 | 2012-10-09 | General Electric Company | Instability mitigation system using stator plasma actuators |
-
2007
- 2007-10-08 FR FR0758130A patent/FR2921978B1/fr active Active
-
2008
- 2008-10-07 JP JP2008260354A patent/JP5512111B2/ja active Active
- 2008-10-07 RU RU2008139862/06A patent/RU2490497C2/ru active
- 2008-10-07 EP EP08165961.7A patent/EP2048329B1/fr active Active
- 2008-10-07 US US12/246,604 patent/US7952244B2/en active Active
- 2008-10-07 CA CA2640048A patent/CA2640048C/fr active Active
Also Published As
Publication number | Publication date |
---|---|
EP2048329B1 (fr) | 2015-08-12 |
CA2640048C (fr) | 2016-09-06 |
RU2490497C2 (ru) | 2013-08-20 |
EP2048329A1 (fr) | 2009-04-15 |
FR2921978B1 (fr) | 2014-04-11 |
RU2008139862A (ru) | 2010-04-20 |
CA2640048A1 (fr) | 2009-04-08 |
JP2009092068A (ja) | 2009-04-30 |
US7952244B2 (en) | 2011-05-31 |
US20090115295A1 (en) | 2009-05-07 |
FR2921978A1 (fr) | 2009-04-10 |
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