FR1483743A - Turbomachine à compresseur contrarotatif - Google Patents

Turbomachine à compresseur contrarotatif

Info

Publication number
FR1483743A
FR1483743A FR40657A FR40657A FR1483743A FR 1483743 A FR1483743 A FR 1483743A FR 40657 A FR40657 A FR 40657A FR 40657 A FR40657 A FR 40657A FR 1483743 A FR1483743 A FR 1483743A
Authority
FR
France
Prior art keywords
contra
turbomachine
rotating compressor
compressor
rotating
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
Application number
FR40657A
Other languages
English (en)
Inventor
Michel Robert Garnier
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Priority to FR40657A priority Critical patent/FR1483743A/fr
Priority to US598422A priority patent/US3385509A/en
Priority to GB53826/66A priority patent/GB1146347A/en
Priority to DE1476907A priority patent/DE1476907C3/de
Application granted granted Critical
Publication of FR1483743A publication Critical patent/FR1483743A/fr
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F01D1/00—Non-positive-displacement machines or engines, e.g. steam turbines
    • F01D1/24—Non-positive-displacement machines or engines, e.g. steam turbines characterised by counter-rotating rotors subjected to same working fluid stream without intermediate stator blades or the like
    • 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
    • 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
    • F01D17/167—Final actuators arranged in stator parts varying effective cross-sectional area of nozzles or guide conduits by means of nozzle vanes of vanes moving in translation
    • 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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/03—Annular blade-carrying members having blades on the inner periphery of the annulus and extending inwardly radially, i.e. inverted rotors
    • 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
    • F01D5/148—Blades with variable camber, e.g. by ejection of fluid
    • 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
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow
    • F02C9/20—Control of working fluid flow by throttling; by adjusting vanes
    • F02C9/22—Control of working fluid flow by throttling; by adjusting vanes by adjusting turbine vanes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D19/00—Axial-flow pumps
    • F04D19/02—Multi-stage pumps
    • F04D19/024—Multi-stage pumps with contrarotating parts
    • 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
    • Y10S415/00—Rotary kinetic fluid motors or pumps
    • Y10S415/914—Device to control boundary layer

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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Positive-Displacement Air Blowers (AREA)
FR40657A 1965-12-02 1965-12-02 Turbomachine à compresseur contrarotatif Expired FR1483743A (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR40657A FR1483743A (fr) 1965-12-02 1965-12-02 Turbomachine à compresseur contrarotatif
US598422A US3385509A (en) 1965-12-02 1966-12-01 Gas turbine engines having contrarotating compressors
GB53826/66A GB1146347A (en) 1965-12-02 1966-12-01 Improvements in or relating to gas turbine engines having contra-rotating compressors
DE1476907A DE1476907C3 (de) 1965-12-02 1966-12-01 Gasturbinentriebwerk mit zwei gleichachsig ineinander angeordneten, drehenden Läufern

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR40657A FR1483743A (fr) 1965-12-02 1965-12-02 Turbomachine à compresseur contrarotatif

Publications (1)

Publication Number Publication Date
FR1483743A true FR1483743A (fr) 1967-06-09

Family

ID=8594145

Family Applications (1)

Application Number Title Priority Date Filing Date
FR40657A Expired FR1483743A (fr) 1965-12-02 1965-12-02 Turbomachine à compresseur contrarotatif

Country Status (4)

Country Link
US (1) US3385509A (fr)
DE (1) DE1476907C3 (fr)
FR (1) FR1483743A (fr)
GB (1) GB1146347A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0735239A1 (fr) * 1995-03-31 1996-10-02 General Electric Company Adaptation de la conception basique d'une turbine à gaz pour l'entraînement de générateurs électriques fonctionnant en fréquences différentes

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1113542A (en) * 1967-01-06 1968-05-15 Rolls Royce Gas turbine engine
US4022542A (en) * 1974-10-23 1977-05-10 Teledyne Industries, Inc. Turbine blade
SE443400B (sv) 1977-12-22 1986-02-24 Garrett Corp Gasturbinmotor samt anvendningen av gasturbinmotorn
US4159624A (en) * 1978-02-06 1979-07-03 Gruner George P Contra-rotating rotors with differential gearing
CA1262409A (fr) * 1985-05-01 1989-10-24 Kenneth Odell Johnson Turbomoteur a contre-rotation
DE3905282C1 (en) * 1987-10-13 1990-05-31 Karl Dipl.-Ing. 2742 Gnarrenburg De Kastens Propeller fan
FR2665223B1 (fr) * 1990-07-26 1994-07-08 Snecma Procede pour entrainer simultanement deux pompes a regimes differents et turbopompe pour comprimer simultanement deux fluides.
US5904470A (en) 1997-01-13 1999-05-18 Massachusetts Institute Of Technology Counter-rotating compressors with control of boundary layers by fluid removal
GB0002257D0 (en) 2000-02-02 2000-03-22 Rolls Royce Plc Rotary apparatus for a gas turbine engine
US6763652B2 (en) * 2002-09-24 2004-07-20 General Electric Company Variable torque split aircraft gas turbine engine counter rotating low pressure turbines
US6763653B2 (en) * 2002-09-24 2004-07-20 General Electric Company Counter rotating fan aircraft gas turbine engine with aft booster
US6763654B2 (en) * 2002-09-30 2004-07-20 General Electric Co. Aircraft gas turbine engine having variable torque split counter rotating low pressure turbines and booster aft of counter rotating fans
CN101903619B (zh) * 2007-12-20 2014-06-11 沃尔沃航空公司 燃气涡轮发动机
RU2376484C1 (ru) * 2008-04-04 2009-12-20 Николай Борисович Болотин Газотурбовоз
EP2508733A1 (fr) 2011-04-07 2012-10-10 Siemens Aktiengesellschaft Turbine à gaz dotée d'un palier de turbine refroidi et procédé de refroidissement du palier de turbine
EP2508711A1 (fr) * 2011-04-07 2012-10-10 Siemens Aktiengesellschaft Palier de turbine axial doté d'un dispositif de sortie d'air et turbine de gaz dotée du palier de turbine axial ainsi que procédé de fonctionnement du palier de turbine axial
US9534608B2 (en) 2012-02-17 2017-01-03 Embry-Riddle Aeronautical University, Inc. Multi-stage axial compressor with counter-rotation
US9353754B2 (en) 2012-03-13 2016-05-31 Embry-Riddle Aeronautical University, Inc. Multi-stage axial compressor with counter-rotation using accessory drive
US9127679B2 (en) * 2012-11-29 2015-09-08 General Electric Company Counter rotating helico-axial pump
WO2015105202A1 (fr) * 2014-01-09 2015-07-16 藤本　広慶 Dispositif de production de poussée
CN107208552B (zh) * 2015-09-09 2020-08-11 苏犁 多轴套传动双向旋转轮扇式涡轮机及镶套轮扇式压气机
US10519976B2 (en) 2017-01-09 2019-12-31 Rolls-Royce Corporation Fluid diodes with ridges to control boundary layer in axial compressor stator vane
CN109737100B (zh) * 2019-01-14 2024-02-02 中国科学院工程热物理研究所 一种抽排气前置导叶与有叶扩压器联合调节装置及方法
US11480111B2 (en) * 2019-05-15 2022-10-25 Honeywell International Inc. Variable area turbine nozzle and method
US12196129B2 (en) * 2021-06-08 2025-01-14 General Electric Company Compressor with counter-rotating blade rows
CN113503264A (zh) * 2021-07-22 2021-10-15 浙江华擎航空发动机科技有限公司 一种采用组合轴系结构的多级压气机
CN114321013B (zh) * 2021-12-15 2023-10-27 山东科技大学 一种基于多对转交截面的无导叶对转压气机及应用

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2505660A (en) * 1950-04-25 Augmentor fob jet propulsion hav
US2505796A (en) * 1942-03-16 1950-05-02 Sedille Marcel Henri Louis System and device for controlling thermal gas turbine motive units
GB586570A (en) * 1943-03-18 1947-03-24 Karl Baumann Improvements in internal combustion turbine plant for propulsion
CH249229A (de) * 1943-06-21 1947-06-15 Jendrassik Georg Verfahren zum Betreiben von mit gasförmigem Arbeitsmittel arbeitenden Strömungsmaschinen und Einrichtung zur Ausführung des Verfahrens.
FR1030483A (fr) * 1951-01-04 1953-06-15 Snecma Procédé et dispositifs de réglage d'un écoulement et leurs diverses applications
GB745693A (en) * 1951-01-04 1956-02-29 Snecma Device for controlling the flow of fluid between cambered blades
US2885856A (en) * 1956-03-23 1959-05-12 Curtiss Wright Corp Apparatus for increasing compressor pressure ratios in a gas turbine engine
GB838602A (en) * 1957-03-06 1960-06-22 Power Jets Res & Dev Ltd Improvements in or relating to gas turbine plant
US3209537A (en) * 1960-05-02 1965-10-05 Bendix Corp Motive fluid control for a re-expansion gas turbine engine
GB985702A (en) * 1960-05-02 1965-03-10 Bendix Corp Gas turbine engine
DE1190737B (de) * 1962-07-27 1965-04-08 Daimler Benz Ag Zweikreis-Gasturbinenstrahltriebwerk
FR1455278A (fr) * 1965-08-05 1966-04-01 Snecma Turboréacteur à double flux

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0735239A1 (fr) * 1995-03-31 1996-10-02 General Electric Company Adaptation de la conception basique d'une turbine à gaz pour l'entraînement de générateurs électriques fonctionnant en fréquences différentes

Also Published As

Publication number Publication date
US3385509A (en) 1968-05-28
DE1476907B2 (de) 1980-09-18
DE1476907C3 (de) 1981-05-21
DE1476907A1 (de) 1969-04-03
GB1146347A (en) 1969-03-26

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