BE766536A - Systeme de refroidissement pour moteurs a turbine a gaz - Google Patents

Systeme de refroidissement pour moteurs a turbine a gaz

Info

Publication number
BE766536A
BE766536A BE766536A BE766536A BE766536A BE 766536 A BE766536 A BE 766536A BE 766536 A BE766536 A BE 766536A BE 766536 A BE766536 A BE 766536A BE 766536 A BE766536 A BE 766536A
Authority
BE
Belgium
Prior art keywords
gas turbine
cooling system
turbine engines
engines
cooling
Prior art date
Application number
BE766536A
Other languages
English (en)
French (fr)
Inventor
D E Uehling
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of BE766536A publication Critical patent/BE766536A/xx

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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • 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
    • Y10S415/00—Rotary kinetic fluid motors or pumps
    • Y10S415/914—Device to control boundary layer

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BE766536A 1970-08-03 1971-04-30 Systeme de refroidissement pour moteurs a turbine a gaz BE766536A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US6032070A 1970-08-03 1970-08-03

Publications (1)

Publication Number Publication Date
BE766536A true BE766536A (fr) 1971-09-16

Family

ID=22028757

Family Applications (1)

Application Number Title Priority Date Filing Date
BE766536A BE766536A (fr) 1970-08-03 1971-04-30 Systeme de refroidissement pour moteurs a turbine a gaz

Country Status (6)

Country Link
US (1) US3632221A (enrdf_load_stackoverflow)
BE (1) BE766536A (enrdf_load_stackoverflow)
CA (1) CA951921A (enrdf_load_stackoverflow)
DE (1) DE2121069A1 (enrdf_load_stackoverflow)
FR (1) FR2101178B1 (enrdf_load_stackoverflow)
GB (1) GB1345910A (enrdf_load_stackoverflow)

Families Citing this family (30)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3897168A (en) * 1974-03-05 1975-07-29 Westinghouse Electric Corp Turbomachine extraction flow guide vanes
US4213738A (en) * 1978-02-21 1980-07-22 General Motors Corporation Cooling air control valve
US4217755A (en) * 1978-12-04 1980-08-19 General Motors Corporation Cooling air control valve
FR2491549B1 (fr) * 1980-10-08 1985-07-05 Snecma Dispositif de refroidissement d'une turbine a gaz, par prelevement d'air au niveau du compresseur
US4397471A (en) * 1981-09-02 1983-08-09 General Electric Company Rotary pressure seal structure and method for reducing thermal stresses therein
DE3638960C1 (de) * 1986-11-14 1988-04-28 Mtu Muenchen Gmbh Gasturbinenstrahltriebwerk mit einem gekuehlten Hochdruckverdichter
EP0267478B1 (de) * 1986-11-14 1991-12-18 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Gasturbinenstrahltriebwerk mit einem Hochdruckverdichter
DE3638961A1 (de) * 1986-11-14 1988-05-26 Mtu Muenchen Gmbh Gasturbinentriebwerk mit einem hochdruckverdichter
FR2609500B1 (fr) * 1987-01-14 1991-04-12 Snecma Disque de compresseur de turbomachine avec accelerateur centripete pour l'aspiration d'air de refroidissement de la turbine
GB2207465B (en) * 1987-07-18 1992-02-19 Rolls Royce Plc A compressor and air bleed arrangement
US5316437A (en) * 1993-02-19 1994-05-31 General Electric Company Gas turbine engine structural frame assembly having a thermally actuated valve for modulating a flow of hot gases through the frame hub
DE19632038A1 (de) * 1996-08-08 1998-02-12 Asea Brown Boveri Vorrichtung zur Abscheidung von Staubpartikeln
US6672072B1 (en) 1998-08-17 2004-01-06 General Electric Company Pressure boosted compressor cooling system
DE10159670A1 (de) * 2001-12-05 2003-06-18 Rolls Royce Deutschland Wirbelgleichrichter im Hochdruckverdichter einer Gasturbine
EP1566531A1 (de) * 2004-02-19 2005-08-24 Siemens Aktiengesellschaft Gasturbine mit einem gegen Auskühlen geschützten Verdichtergehäuse und Verfahren zum Betrieb einer Gasturbine
DE102004042295A1 (de) * 2004-09-01 2006-03-02 Mtu Aero Engines Gmbh Rotor für ein Triebwerk
US7331763B2 (en) * 2005-12-20 2008-02-19 General Electric Company Turbine disk
US8578716B2 (en) * 2008-03-22 2013-11-12 United Technologies Corporation Valve system for a gas turbine engine
US8636910B2 (en) 2010-08-24 2014-01-28 Qwtip Llc Water treatment and revitalization system and method
US10790723B2 (en) 2010-08-24 2020-09-29 Qwtip Llc Disk-pack turbine
US9605663B2 (en) 2010-08-24 2017-03-28 Qwtip Llc System and method for separating fluids and creating magnetic fields
US9469553B2 (en) 2011-08-24 2016-10-18 Qwtip, Llc Retrofit attachments for water treatment systems
AR088431A1 (es) 2011-08-24 2014-06-11 Qwtip Llc Sistema y metodo de tratamiento de agua
MX352753B (es) 2011-08-24 2017-12-07 Qwtip Llc Sistema y método de tratamiento de agua.
AR093196A1 (es) 2012-02-28 2015-05-27 Qwtip Llc Sistema y metodo de desalinizacion y/o produccion de gas
AR093197A1 (es) 2012-02-29 2015-05-27 Qwtip Llc Sistema y metodo de levitacion y distribucion
US9091173B2 (en) 2012-05-31 2015-07-28 United Technologies Corporation Turbine coolant supply system
US9617917B2 (en) 2013-07-31 2017-04-11 General Electric Company Flow control assembly and methods of assembling the same
US11149642B2 (en) 2015-12-30 2021-10-19 General Electric Company System and method of reducing post-shutdown engine temperatures
US10822100B2 (en) * 2017-06-26 2020-11-03 General Electric Company Hybrid electric propulsion system for an aircraft

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2618433A (en) * 1948-06-23 1952-11-18 Curtiss Wright Corp Means for bleeding air from compressors
US2791091A (en) * 1950-05-15 1957-05-07 Gen Motors Corp Power plant cooling and thrust balancing systems
GB712051A (en) * 1951-10-10 1954-07-14 Rolls Royce Improvements in or relating to axial-flow fluid machines
US2787440A (en) * 1953-05-21 1957-04-02 Westinghouse Electric Corp Turbine apparatus
US3043561A (en) * 1958-12-29 1962-07-10 Gen Electric Turbine rotor ventilation system
CH487337A (de) * 1968-01-10 1970-03-15 Sulzer Ag Anordnung für den Durchtritt von Gas durch den Mantel eines hohlen Rotors

Also Published As

Publication number Publication date
FR2101178A1 (enrdf_load_stackoverflow) 1972-03-31
FR2101178B1 (enrdf_load_stackoverflow) 1974-04-05
DE2121069A1 (de) 1972-02-10
US3632221A (en) 1972-01-04
CA951921A (en) 1974-07-30
GB1345910A (en) 1974-02-06

Similar Documents

Publication Publication Date Title
BE766536A (fr) Systeme de refroidissement pour moteurs a turbine a gaz
BE773357A (fr) Systeme de combustion a fente annulaire pour moteurs a turbine a gaz
BE860915A (fr) Systeme de refroidissement perfectionne pour moteur a turbine a gaz
BE746282A (fr) Moteurs a turbine a gaz perfectionnes
BE744919A (fr) Moteurs a turbine a gaz perfectionnes
BE825974A (fr) Systeme de refroidissement de turbine a gaz
FR2336554A1 (fr) Systeme de combustion pour turbines a gaz
CA994116A (en) Pin-fin cooling system for a gas turbine engine
FR95211E (fr) Structure de bati pour moteur a turbine a gaz.
BE820469A (fr) Systeme anti-decrochage pour turbine a gaz
AU3490971A (en) Wall structure for a gas turbine engine
IT998522B (it) Apparato di combustione per motori a turbina a gas
BE787374A (fr) Systeme de drainage de combustible pour moteur a turbine a gaz
BE756363A (fr) Systeme d'echappement pour compresseurs de moteurs a turbine a gaz
BE812506A (fr) Perfectionnements aux systemes de combustion pour moteurs a turbinea gaz
FR1421829A (fr) équipement de combustion pour moteur à turbine à gaz
BE755508A (fr) Rotor pour moteurs a turbine a gaz
CA702551A (en) Lubrication system for gas turbine engine
FR1493144A (fr) Perfectionnements aux appareils de combustion pour moteurs de turbines à gaz
FR1507471A (fr) Structure de bâti pour moteur à turbine à gaz
BE775776R (fr) Systeme de combustion perfectionne pour moteurs a combustion
IL41441A0 (en) Cooling system for internal combustion engines
YU162971A (en) Exhausting system for internal combustion engines
FR1373323A (fr) Système de démarrage pour moteurs à turbines à gaz
FR1389254A (fr) Compresseur pour moteur à turbine à gaz