BE766536A - COOLING SYSTEM FOR GAS TURBINE ENGINES - Google Patents

COOLING SYSTEM FOR GAS TURBINE ENGINES

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
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/en

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)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
BE766536A 1970-08-03 1971-04-30 COOLING SYSTEM FOR GAS TURBINE ENGINES BE766536A (en)

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 (en) 1971-09-16

Family

ID=22028757

Family Applications (1)

Application Number Title Priority Date Filing Date
BE766536A BE766536A (en) 1970-08-03 1971-04-30 COOLING SYSTEM FOR GAS TURBINE ENGINES

Country Status (6)

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

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 (en) * 1980-10-08 1985-07-05 Snecma DEVICE FOR COOLING A GAS TURBINE, BY TAKING AIR FROM THE COMPRESSOR
US4397471A (en) * 1981-09-02 1983-08-09 General Electric Company Rotary pressure seal structure and method for reducing thermal stresses therein
EP0267478B1 (en) * 1986-11-14 1991-12-18 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Gas turbine jet engine with a high pressure compressor
DE3638961A1 (en) * 1986-11-14 1988-05-26 Mtu Muenchen Gmbh GAS TURBINE ENGINE WITH A HIGH PRESSURE COMPRESSOR
DE3638960C1 (en) * 1986-11-14 1988-04-28 Mtu Muenchen Gmbh Gas turbine jet engine with a cooled high pressure compressor
FR2609500B1 (en) * 1987-01-14 1991-04-12 Snecma TURBOMACHINE COMPRESSOR DISC WITH CENTRIPTIC ACCELERATOR FOR SUCTION OF TURBINE COOLING AIR
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 (en) * 1996-08-08 1998-02-12 Asea Brown Boveri Device for separating dust particles
US6672072B1 (en) 1998-08-17 2004-01-06 General Electric Company Pressure boosted compressor cooling system
DE10159670A1 (en) * 2001-12-05 2003-06-18 Rolls Royce Deutschland Vortex rectifier in the high pressure compressor of a gas turbine
EP1566531A1 (en) * 2004-02-19 2005-08-24 Siemens Aktiengesellschaft Gas turbine with compressor casing protected against cooling and Method to operate a gas turbine
DE102004042295A1 (en) * 2004-09-01 2006-03-02 Mtu Aero Engines Gmbh Rotor for an engine
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
KR20140079379A (en) 2011-08-24 2014-06-26 큐더블유티아이피 엘엘씨 Water treatment system and method
TW201323047A (en) 2011-08-24 2013-06-16 Qwtip Llc Water treatment system and method
AR093196A1 (en) 2012-02-28 2015-05-27 Qwtip Llc SYSTEM AND METHOD OF DESALINATION AND / OR GAS PRODUCTION
AR093197A1 (en) 2012-02-29 2015-05-27 Qwtip Llc SYSTEM AND METHOD OF LEVITATION AND DISTRIBUTION
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 (en) * 1968-01-10 1970-03-15 Sulzer Ag Arrangement for the passage of gas through the shell of a hollow rotor

Also Published As

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

Similar Documents

Publication Publication Date Title
BE766536A (en) COOLING SYSTEM FOR GAS TURBINE ENGINES
BE860915A (en) ADVANCED COOLING SYSTEM FOR GAS TURBINE ENGINES
BE746282A (en) ADVANCED GAS TURBINE ENGINES
BE825974A (en) GAS TURBINE COOLING SYSTEM
BE744919A (en) ADVANCED GAS TURBINE ENGINES
FR2336554A1 (en) COMBUSTION SYSTEM FOR GAS TURBINES
BE773357A (en) ANNULAR SLOT COMBUSTION SYSTEM FOR GAS TURBINE ENGINES
CA994116A (en) Pin-fin cooling system for a gas turbine engine
FR95211E (en) Frame structure for gas turbine engine.
IT998522B (en) COMBUSTION EQUIPMENT FOR GAS TURBINE ENGINES
IL37773A (en) Wall structure for a gas turbine engine
BE787374A (en) FUEL DRAINAGE SYSTEM FOR GAS TURBINE ENGINES
BE756363A (en) EXHAUST SYSTEM FOR COMPRESSORS OF GAS TURBINE ENGINES
BE812506A (en) IMPROVEMENTS TO COMBUSTION SYSTEMS FOR GAS TURBINE ENGINES
BE757185A (en) EXHAUST GAS EXHAUST SYSTEM FOR INTERNAL COMBUSTION ENGINES
FR1421829A (en) combustion equipment for gas turbine engine
BE755508A (en) ROTOR FOR GAS TURBINE ENGINES
CA702551A (en) Lubrication system for gas turbine engine
FR1493144A (en) Improvements to combustion devices for gas turbine engines
FR1507471A (en) Frame structure for gas turbine engine
BE775776R (en) PERFECTED COMBUSTION SYSTEM FOR COMBUSTION ENGINES
FR1385923A (en) New bearing system, especially for gas turbine engines
IL41441A0 (en) Cooling system for internal combustion engines
FR1373323A (en) Starting system for gas turbine engines
FR1389254A (en) Compressor for gas turbine engine