FR2158461A1 - - Google Patents

Info

Publication number
FR2158461A1
FR2158461A1 FR7238822A FR7238822A FR2158461A1 FR 2158461 A1 FR2158461 A1 FR 2158461A1 FR 7238822 A FR7238822 A FR 7238822A FR 7238822 A FR7238822 A FR 7238822A FR 2158461 A1 FR2158461 A1 FR 2158461A1
Authority
FR
France
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.)
Granted
Application number
FR7238822A
Other versions
FR2158461B1 (fr
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of FR2158461A1 publication Critical patent/FR2158461A1/fr
Application granted granted Critical
Publication of FR2158461B1 publication Critical patent/FR2158461B1/fr
Expired legal-status Critical Current

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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
    • 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
    • F02C3/08—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising at least one radial stage
    • 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
    • F02K3/068—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 being characterised by a short axial length relative to the diameter
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/52—Toroidal combustion chambers
    • 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

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)
FR7238822A 1971-11-05 1972-11-02 Expired FR2158461B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB5160771A GB1361036A (en) 1971-11-05 1971-11-05 Gas turbine ducted fan propulsion unit

Publications (2)

Publication Number Publication Date
FR2158461A1 true FR2158461A1 (fr) 1973-06-15
FR2158461B1 FR2158461B1 (fr) 1977-03-18

Family

ID=10460690

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7238822A Expired FR2158461B1 (fr) 1971-11-05 1972-11-02

Country Status (5)

Country Link
US (1) US3892069A (fr)
JP (1) JPS4992417A (fr)
DE (1) DE2253935A1 (fr)
FR (1) FR2158461B1 (fr)
GB (1) GB1361036A (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0079149A1 (fr) * 1981-10-22 1983-05-18 Gaston Lavoie Turbine à gaz avec chambre de combustion toroidale
EP2791489B1 (fr) * 2011-12-15 2020-02-05 Siemens Energy, Inc. Turbine à gaz à flux radial dotée d'un conduit de transition avancé
CN111396927A (zh) * 2020-03-27 2020-07-10 中国科学院工程热物理研究所 二维阵列无传统旋流器的低污染燃烧装置

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4230014C1 (de) * 1992-09-08 1994-03-24 Eberspaecher J Vorrichtung zur Reduzierung der Geräuschentwicklung bei Gebläsen
GB2301630B (en) * 1995-06-01 1999-12-29 Bridge Butler James Alexander Internal combustion turbine engine
US6430917B1 (en) * 2001-02-09 2002-08-13 The Regents Of The University Of California Single rotor turbine engine
US20030192303A1 (en) * 2002-04-15 2003-10-16 Paul Marius A. Integrated bypass turbojet engines for aircraft and other vehicles
US6966174B2 (en) * 2002-04-15 2005-11-22 Paul Marius A Integrated bypass turbojet engines for air craft and other vehicles
WO2004092567A2 (fr) * 2002-04-15 2004-10-28 Marius Paul A Turboreacteurs a derivation integree destines a des aeronefs et a d'autres vehicules
US7044718B1 (en) 2003-07-08 2006-05-16 The Regents Of The University Of California Radial-radial single rotor turbine
US8181902B2 (en) 2005-03-15 2012-05-22 Entecho Pty Ltd. Aerodynamic lifting device and airborne craft
US7556218B2 (en) 2005-03-15 2009-07-07 Entecho Pty Ltd. Aerodynamic lifting device and airborne craft
US20070022738A1 (en) * 2005-07-27 2007-02-01 United Technologies Corporation Reinforcement rings for a tip turbine engine fan-turbine rotor assembly
EP1969222B1 (fr) * 2005-12-12 2012-11-21 United Technologies Corporation Structure de type palier pour maitriser les deflections d'un composant rotatif
US8356469B1 (en) 2007-04-05 2013-01-22 The United States Of America As Represented By The Secretary Of The Air Force Gas turbine engine with dual compression rotor
AU2008202134A1 (en) * 2007-05-16 2008-12-04 Entecho Pty Ltd Thrust Vectoring Shroud for Fluid Dynamic Device
EP2274204B1 (fr) * 2008-05-07 2014-10-15 Entecho Pty.Ltd. Engin aerien avec un dispositif fluidique avec un carennage de commande de poussée
CN101798958A (zh) * 2009-02-06 2010-08-11 余志刚 内涵道涡轮风扇发动机
CN101936239A (zh) * 2009-06-30 2011-01-05 余志刚 离心式转子风扇发动机
JP6357707B2 (ja) 2013-07-01 2018-07-18 エンテコー ピーティーワイ リミテッドＥｎｔｅｃｈｏ Ｐｔｙ Ｌｔｄ 空力揚力装置
CN105197231B (zh) * 2015-10-30 2017-11-07 佛山市神风航空科技有限公司 一种方便调整推力方向的装置
IL268133B (en) * 2017-01-20 2022-08-01 Maran John Vedamanikam A vtol plane with thrust rising from a central fan
DE102017119070B4 (de) 2017-08-21 2021-03-11 Finn Schöning Strahltriebwerk
US11536456B2 (en) * 2017-10-24 2022-12-27 General Electric Company Fuel and air injection handling system for a combustor of a rotating detonation engine
CN108049985B (zh) * 2018-01-29 2020-05-08 余四艳 旋喷式可变循环航空喷气发动机
CN108361109B (zh) * 2018-01-29 2020-08-11 余四艳 通用型宽能源旋喷发动机
CN108518282A (zh) * 2018-03-30 2018-09-11 余四艳 大功率宽能源旋喷式多缸燃气发动机
CN112081661A (zh) * 2019-06-12 2020-12-15 程浩鹏 一种外环涡轮风扇发动机
CN112081684A (zh) * 2019-06-12 2020-12-15 程浩鹏 一种喷气风扇发动机
CN110588969B (zh) * 2019-10-01 2023-05-19 重庆碟翔航空科技有限公司 一种三维可变推进飞碟
CN111810243B (zh) * 2020-07-17 2022-09-27 南昌航空大学 一种压气机-涡轮一体化发动机

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2689681A (en) * 1949-09-17 1954-09-21 United Aircraft Corp Reversely rotating screw type multiple impeller compressor
DE1000189B (de) * 1955-06-28 1957-01-03 Bmw Studiengesellschaft Fuer T Gasturbine, insbesondere Kleingasturbine
US3283509A (en) * 1963-02-21 1966-11-08 Messerschmitt Boelkow Blohm Lifting engine for vtol aircraft
US3269120A (en) * 1964-07-16 1966-08-30 Curtiss Wright Corp Gas turbine engine with compressor and turbine passages in a single rotor element
US3310940A (en) * 1965-10-07 1967-03-28 Stalker Corp Gas turbines
US3603082A (en) * 1970-02-18 1971-09-07 Curtiss Wright Corp Combustor for gas turbine having a compressor and turbine passages in a single rotor element

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
NEANT *

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0079149A1 (fr) * 1981-10-22 1983-05-18 Gaston Lavoie Turbine à gaz avec chambre de combustion toroidale
EP2791489B1 (fr) * 2011-12-15 2020-02-05 Siemens Energy, Inc. Turbine à gaz à flux radial dotée d'un conduit de transition avancé
CN111396927A (zh) * 2020-03-27 2020-07-10 中国科学院工程热物理研究所 二维阵列无传统旋流器的低污染燃烧装置

Also Published As

Publication number Publication date
DE2253935A1 (de) 1973-05-10
FR2158461B1 (fr) 1977-03-18
US3892069A (en) 1975-07-01
GB1361036A (en) 1974-07-24
JPS4992417A (fr) 1974-09-03

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Legal Events

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