FR2617907B1 - Moteur a turbine a gaz - Google Patents
Moteur a turbine a gazInfo
- Publication number
- FR2617907B1 FR2617907B1 FR8803635A FR8803635A FR2617907B1 FR 2617907 B1 FR2617907 B1 FR 2617907B1 FR 8803635 A FR8803635 A FR 8803635A FR 8803635 A FR8803635 A FR 8803635A FR 2617907 B1 FR2617907 B1 FR 2617907B1
- Authority
- FR
- France
- Prior art keywords
- gas turbine
- turbine engine
- engine
- gas
- turbine
- 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 - Lifetime
Links
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
- F02K3/072—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 counter-rotating, e.g. fan rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
- B64C11/46—Arrangements of, or constructional features peculiar to, multiple propellers
- B64C11/48—Units of two or more coaxial propellers
-
- 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
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/141—Shape, i.e. outer, aerodynamic form
- F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
-
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/06—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
- F02C3/067—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages having counter-rotating rotors
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S416/00—Fluid reaction surfaces, i.e. impellers
- Y10S416/02—Formulas of curves
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)
- Aviation & Aerospace Engineering (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US7002087A | 1987-07-06 | 1987-07-06 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2617907A1 FR2617907A1 (fr) | 1989-01-13 |
FR2617907B1 true FR2617907B1 (fr) | 1994-04-08 |
Family
ID=22092619
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8803635A Expired - Lifetime FR2617907B1 (fr) | 1987-07-06 | 1988-03-21 | Moteur a turbine a gaz |
Country Status (7)
Country | Link |
---|---|
US (1) | US4809498A (fr) |
JP (1) | JP3062199B2 (fr) |
DE (1) | DE3814971C2 (fr) |
FR (1) | FR2617907B1 (fr) |
GB (1) | GB2207191B (fr) |
IT (1) | IT1216047B (fr) |
SE (1) | SE466558B (fr) |
Families Citing this family (74)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4951461A (en) * | 1989-03-20 | 1990-08-28 | General Electric Company | Power turbine support arrangement |
US5112191A (en) * | 1989-04-11 | 1992-05-12 | General Electric Company | Rotating cowling |
US5156525A (en) * | 1991-02-26 | 1992-10-20 | General Electric Company | Turbine assembly |
DE4122008A1 (de) * | 1991-07-03 | 1993-01-14 | Mtu Muenchen Gmbh | Propfantriebwerk mit gegenlaeufigem niederdruckverdichter (booster) |
US5388964A (en) * | 1993-09-14 | 1995-02-14 | General Electric Company | Hybrid rotor blade |
US5904470A (en) * | 1997-01-13 | 1999-05-18 | Massachusetts Institute Of Technology | Counter-rotating compressors with control of boundary layers by fluid removal |
EP0952330A3 (fr) * | 1998-04-13 | 2000-05-24 | Nikkiso Company, Ltd. | Turbosoufflante avec soufflante à vitesse réduite |
EP0950808A3 (fr) * | 1998-04-13 | 2000-05-24 | Nikkiso Company, Ltd. | Turboréacteur à double flux avec soufflante à vitesse réduite |
US6209311B1 (en) | 1998-04-13 | 2001-04-03 | Nikkiso Company, Ltd. | Turbofan engine including fans with reduced speed |
JP2000303854A (ja) * | 1999-04-23 | 2000-10-31 | Eruson Kk | 高効率ガスタービン |
JP2002213206A (ja) * | 2001-01-12 | 2002-07-31 | Mitsubishi Heavy Ind Ltd | ガスタービンにおける翼構造 |
JP4373629B2 (ja) * | 2001-08-31 | 2009-11-25 | 株式会社東芝 | 軸流タービン |
US6619030B1 (en) | 2002-03-01 | 2003-09-16 | General Electric Company | Aircraft engine with inter-turbine engine frame supported counter rotating low pressure turbine rotors |
US6732502B2 (en) | 2002-03-01 | 2004-05-11 | General Electric Company | Counter rotating aircraft gas turbine engine with high overall pressure ratio compressor |
DE10306820A1 (de) * | 2003-02-19 | 2004-09-02 | Mtu Aero Engines Gmbh | Anordnung zur Beeinflussung des Wärmeübergangs in rotierenden Einrichtungen, insbesondere in Gasturbinen |
GB0406174D0 (en) | 2004-03-19 | 2004-04-21 | Rolls Royce Plc | Turbine engine arrangement |
US7594388B2 (en) * | 2005-06-06 | 2009-09-29 | General Electric Company | Counterrotating turbofan engine |
US7645115B2 (en) * | 2006-04-03 | 2010-01-12 | Abraham Daniel Schneider | System, method, and apparatus for a power producing linear fluid impulse machine |
US20080075590A1 (en) * | 2006-09-27 | 2008-03-27 | Thomas Ory Moniz | Gas turbine engine assembly and method of assembling same |
US7921634B2 (en) * | 2006-10-31 | 2011-04-12 | General Electric Company | Turbofan engine assembly and method of assembling same |
US7765789B2 (en) * | 2006-12-15 | 2010-08-03 | General Electric Company | Apparatus and method for assembling gas turbine engines |
FR2912181B1 (fr) * | 2007-02-07 | 2009-04-24 | Snecma Sa | Turbine a gaz a turbines hp et bp contra-rotatives |
US8038388B2 (en) | 2007-03-05 | 2011-10-18 | United Technologies Corporation | Abradable component for a gas turbine engine |
US20100229568A1 (en) * | 2007-08-02 | 2010-09-16 | Kevork Nercessian | Gas turbine engine |
GB0809759D0 (en) * | 2008-05-30 | 2008-07-09 | Rolls Royce Plc | Gas turbine engine |
US20140174056A1 (en) | 2008-06-02 | 2014-06-26 | United Technologies Corporation | Gas turbine engine with low stage count low pressure turbine |
US8128021B2 (en) | 2008-06-02 | 2012-03-06 | United Technologies Corporation | Engine mount system for a turbofan gas turbine engine |
DE102010014900A1 (de) * | 2010-04-14 | 2011-10-20 | Rolls-Royce Deutschland Ltd & Co Kg | Nebenstromkanal eines Turbofantriebwerkes |
US8453445B2 (en) * | 2010-04-19 | 2013-06-04 | Honeywell International Inc. | Axial turbine with parallel flow compressor |
US8453448B2 (en) * | 2010-04-19 | 2013-06-04 | Honeywell International Inc. | Axial turbine |
US8353161B2 (en) * | 2010-04-19 | 2013-01-15 | Honeywell International Inc. | High diffusion turbine wheel with hub bulb |
EP2458149B1 (fr) * | 2010-11-30 | 2020-04-08 | MTU Aero Engines GmbH | Aubage pour turboréacteur |
FR2970746B1 (fr) * | 2011-01-20 | 2015-12-04 | Snecma | Turbomachine a turbines haute pression et basse pression imbriquees |
US9631558B2 (en) | 2012-01-03 | 2017-04-25 | United Technologies Corporation | Geared architecture for high speed and small volume fan drive turbine |
US9239012B2 (en) | 2011-06-08 | 2016-01-19 | United Technologies Corporation | Flexible support structure for a geared architecture gas turbine engine |
US20130192201A1 (en) * | 2012-01-31 | 2013-08-01 | United Technologies Corporation | Geared turbofan gas turbine engine architecture |
US9816442B2 (en) | 2012-01-31 | 2017-11-14 | United Technologies Corporation | Gas turbine engine with high speed low pressure turbine section |
US8887487B2 (en) * | 2012-01-31 | 2014-11-18 | United Technologies Corporation | Geared turbofan gas turbine engine architecture |
US9222417B2 (en) | 2012-01-31 | 2015-12-29 | United Technologies Corporation | Geared turbofan gas turbine engine architecture |
US9611859B2 (en) | 2012-01-31 | 2017-04-04 | United Technologies Corporation | Gas turbine engine with high speed low pressure turbine section and bearing support features |
US20150345426A1 (en) | 2012-01-31 | 2015-12-03 | United Technologies Corporation | Geared turbofan gas turbine engine architecture |
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 |
US20130192191A1 (en) | 2012-01-31 | 2013-08-01 | Frederick M. Schwarz | Gas turbine engine with high speed low pressure turbine section and bearing support features |
US8935913B2 (en) | 2012-01-31 | 2015-01-20 | United Technologies Corporation | Geared turbofan gas turbine engine architecture |
US10240526B2 (en) | 2012-01-31 | 2019-03-26 | United Technologies Corporation | Gas turbine engine with high speed low pressure turbine section |
US20130192265A1 (en) * | 2012-01-31 | 2013-08-01 | Frederick M. Schwarz | Gas turbine engine with high speed low pressure turbine section and bearing support features |
US10125693B2 (en) | 2012-04-02 | 2018-11-13 | United Technologies Corporation | Geared turbofan engine with power density range |
EP2841718A4 (fr) * | 2012-04-25 | 2016-03-02 | United Technologies Corp | Moteur à turbine à gaz présentant une section de turbine basse pression à grande vitesse et éléments de support de palier |
US8756908B2 (en) | 2012-05-31 | 2014-06-24 | United Technologies Corporation | Fundamental gear system architecture |
US20150308351A1 (en) | 2012-05-31 | 2015-10-29 | United Technologies Corporation | Fundamental gear system architecture |
US8572943B1 (en) | 2012-05-31 | 2013-11-05 | United Technologies Corporation | Fundamental gear system architecture |
US9512721B2 (en) | 2012-07-20 | 2016-12-06 | Pratt & Whitney Canada Corp. | Compound cycle engine |
US10107195B2 (en) | 2012-07-20 | 2018-10-23 | Pratt & Whitney Canada Corp. | Compound cycle engine |
US9926843B2 (en) | 2012-07-20 | 2018-03-27 | Pratt & Whitney Canada Corp. | Compound cycle engine |
US20140072433A1 (en) * | 2012-09-10 | 2014-03-13 | General Electric Company | Method of clocking a turbine by reshaping the turbine's downstream airfoils |
BR112015017110A2 (pt) * | 2013-01-18 | 2017-07-11 | Gen Electric | motor de turbina a gás |
US10724479B2 (en) | 2013-03-15 | 2020-07-28 | United Technologies Corporation | Thrust efficient turbofan engine |
US9624827B2 (en) | 2013-03-15 | 2017-04-18 | United Technologies Corporation | Thrust efficient turbofan engine |
US9435221B2 (en) | 2013-08-09 | 2016-09-06 | General Electric Company | Turbomachine airfoil positioning |
WO2015130386A2 (fr) * | 2013-12-12 | 2015-09-03 | United Technologies Corporation | Turbomachine à vitesse relative élevée |
JP6166201B2 (ja) * | 2014-03-13 | 2017-07-19 | 竹田 眞司 | 圧縮回転羽がそれぞれ逆回転して燃焼排出回転羽がそれぞれ逆回転して、圧縮を強くして燃焼を強めるジェットエンジンとガスタ−ビンエンジン、 |
JP6396093B2 (ja) * | 2014-06-26 | 2018-09-26 | 三菱重工業株式会社 | タービン動翼列、タービン段落及び軸流タービン |
US20160195010A1 (en) * | 2014-07-15 | 2016-07-07 | United Technologies Corporation | Vaneless counterrotating turbine |
US10655471B2 (en) * | 2015-02-10 | 2020-05-19 | Mitsubishi Hitachi Power Systems, Ltd. | Turbine and gas turbine |
US20170138202A1 (en) * | 2015-11-16 | 2017-05-18 | General Electric Company | Optimal lift designs for gas turbine engines |
CN106801620B (zh) * | 2015-11-25 | 2019-03-22 | 熵零股份有限公司 | 一种对转冲压叶轮机构 |
CN106917638B (zh) * | 2015-12-24 | 2019-03-22 | 熵零股份有限公司 | 一种对转冲压叶轮机构 |
US11428241B2 (en) * | 2016-04-22 | 2022-08-30 | Raytheon Technologies Corporation | System for an improved stator assembly |
US10422348B2 (en) | 2017-01-10 | 2019-09-24 | General Electric Company | Unsymmetrical turbofan abradable grind for reduced rub loads |
US10876407B2 (en) * | 2017-02-16 | 2020-12-29 | General Electric Company | Thermal structure for outer diameter mounted turbine blades |
US10723470B2 (en) * | 2017-06-12 | 2020-07-28 | Raytheon Technologies Corporation | Aft fan counter-rotating turbine engine |
US11428160B2 (en) | 2020-12-31 | 2022-08-30 | General Electric Company | Gas turbine engine with interdigitated turbine and gear assembly |
CN113250754B (zh) * | 2021-04-22 | 2023-05-05 | 中国民用航空飞行学院 | 一种对转盘腔流动结构 |
US12017751B2 (en) | 2021-09-15 | 2024-06-25 | General Electric Company | Inlet for unducted propulsion system |
Family Cites Families (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2505660A (en) * | 1950-04-25 | Augmentor fob jet propulsion hav | ||
BE334235A (fr) * | 1925-05-27 | 1926-05-21 | ||
US2378372A (en) * | 1937-12-15 | 1945-06-12 | Whittle Frank | Turbine and compressor |
US2455458A (en) * | 1940-03-02 | 1948-12-07 | Power Jets Res & Dev Ltd | Thrust augmenting device for a system for developing propulsive thrust |
US2477798A (en) * | 1941-04-08 | 1949-08-02 | Rolls Royce | Contrarotating axial flow high and low pressure turbine and compressor with bladed duct with turbine cooling |
US2428330A (en) * | 1943-01-15 | 1947-09-30 | Armstrong Siddeley Motors Ltd | Assembly of multistage internalcombustion turbines embodying contrarotating bladed members |
US2454738A (en) * | 1944-01-31 | 1948-11-23 | Power Jets Res And Development | Internal-combustion turbine power plant |
US2471892A (en) * | 1944-02-14 | 1949-05-31 | Lockheed Aircraft Corp | Reactive propulsion power plant having radial flow compressor and turbine means |
US2575682A (en) * | 1944-02-14 | 1951-11-20 | Lockheed Aircraft Corp | Reaction propulsion aircraft power plant having independently rotating compressor and turbine blading stages |
US2478206A (en) * | 1944-02-24 | 1949-08-09 | Westinghouse Electric Corp | Multirotor gas turbine power plant with propeller |
US2488783A (en) * | 1945-03-12 | 1949-11-22 | Edward A Stalker | Gas turbine |
GB612838A (en) * | 1945-04-04 | 1948-11-18 | Lysholm Alf | Improvements in or relating to moving blades for elastic fluid turbines |
US2639583A (en) * | 1947-06-25 | 1953-05-26 | Harry C Steele | Contrarotating gas turbine having a power turbine and a plurality of compressor-turbines in series |
GB665916A (en) * | 1948-10-01 | 1952-02-06 | Plessey Co Ltd | A cordite operated starter turbine |
US2608821A (en) * | 1949-10-08 | 1952-09-02 | Gen Electric | Contrarotating turbojet engine having independent bearing supports for each turbocompressor |
BE529689A (fr) * | 1953-06-18 | |||
GB800602A (en) * | 1955-03-16 | 1958-08-27 | Bristol Aero Engines Ltd | Improvements in or relating to jet propulsion gas turbine engines |
CH379837A (de) * | 1959-09-16 | 1964-07-15 | Maschf Augsburg Nuernberg Ag | Schaufelung für axial durchströmte Turbinen, insbesondere Gasturbinen |
US3363419A (en) * | 1965-04-27 | 1968-01-16 | Rolls Royce | Gas turbine ducted fan engine |
US3381475A (en) * | 1965-06-28 | 1968-05-07 | Bristol Siddeley Engines Ltd | Jet propulsion engines |
US3797239A (en) * | 1965-10-24 | 1974-03-19 | United Aircraft Corp | Supersonic combustion engine |
US3475108A (en) * | 1968-02-14 | 1969-10-28 | Siemens Ag | Blade structure for turbines |
US3635576A (en) * | 1970-04-20 | 1972-01-18 | Gerhard Wieckmann | Turbine structure |
US3703081A (en) * | 1970-11-20 | 1972-11-21 | Gen Electric | Gas turbine engine |
US3861139A (en) * | 1973-02-12 | 1975-01-21 | Gen Electric | Turbofan engine having counterrotating compressor and turbine elements and unique fan disposition |
US4159624A (en) * | 1978-02-06 | 1979-07-03 | Gruner George P | Contra-rotating rotors with differential gearing |
US4571935A (en) * | 1978-10-26 | 1986-02-25 | Rice Ivan G | Process for steam cooling a power turbine |
FR2506840A1 (fr) * | 1981-05-29 | 1982-12-03 | Onera (Off Nat Aerospatiale) | Turboreacteur a roues contra-rotatives |
NL8303401A (nl) * | 1982-11-01 | 1984-06-01 | Gen Electric | Aandrijfturbine voor tegengesteld draaiende propellers. |
FR2560642A1 (fr) * | 1984-03-02 | 1985-09-06 | Gen Electric | Moteur a turbosoufflante a contre-rotation |
-
1988
- 1988-03-07 GB GB8805368A patent/GB2207191B/en not_active Expired - Lifetime
- 1988-03-10 IT IT8819721A patent/IT1216047B/it active
- 1988-03-21 FR FR8803635A patent/FR2617907B1/fr not_active Expired - Lifetime
- 1988-03-23 JP JP63067500A patent/JP3062199B2/ja not_active Expired - Lifetime
- 1988-05-03 DE DE3814971A patent/DE3814971C2/de not_active Expired - Fee Related
- 1988-06-20 US US07/208,803 patent/US4809498A/en not_active Expired - Lifetime
- 1988-09-27 SE SE8803415A patent/SE466558B/sv not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
SE8803415L (sv) | 1990-03-28 |
SE466558B (sv) | 1992-03-02 |
DE3814971C2 (de) | 2002-01-24 |
GB2207191A (en) | 1989-01-25 |
DE3814971A1 (de) | 1989-01-19 |
IT1216047B (it) | 1990-02-22 |
IT8819721A0 (it) | 1988-03-10 |
FR2617907A1 (fr) | 1989-01-13 |
GB8805368D0 (en) | 1988-04-07 |
US4809498A (en) | 1989-03-07 |
JP3062199B2 (ja) | 2000-07-10 |
SE8803415D0 (sv) | 1988-09-27 |
GB2207191B (en) | 1992-03-04 |
JPS6412005A (en) | 1989-01-17 |
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