GB791232A - Improvements in or relating to gas turbine power plants - Google Patents

Improvements in or relating to gas turbine power plants

Info

Publication number
GB791232A
GB791232A GB2421954A GB2421954A GB791232A GB 791232 A GB791232 A GB 791232A GB 2421954 A GB2421954 A GB 2421954A GB 2421954 A GB2421954 A GB 2421954A GB 791232 A GB791232 A GB 791232A
Authority
GB
United Kingdom
Prior art keywords
combustion chamber
annular
gas turbine
velocity
sheet metal
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
GB2421954A
Inventor
Rudolph Birmann
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.)
DE LAVAL STEAM TURBINE CO
Original Assignee
DE LAVAL STEAM TURBINE CO
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 DE LAVAL STEAM TURBINE CO filed Critical DE LAVAL STEAM TURBINE CO
Priority to GB2421954A priority Critical patent/GB791232A/en
Publication of GB791232A publication Critical patent/GB791232A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/045Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor-module
    • F02C3/05Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor having compressor and turbine passages in a single rotor-module the compressor and the turbine being of the radial flow type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/12Cooling of plants
    • F02C7/16Cooling of plants characterised by cooling medium
    • F02C7/18Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies
    • Y02T50/67Relevant aircraft propulsion technologies
    • Y02T50/671Measures to reduce the propulsor weight
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies
    • Y02T50/67Relevant aircraft propulsion technologies
    • Y02T50/675Enabling an increased combustion temperature by cooling

Abstract

791,232. Generating combustion products under pressure. DE LAVAL STEAM TURBINE CO. Aug. 19, 1954, No. 24219/54. Class 51 (1). [Also in Group XXVI] Fig. 1 shows a gas turbine plant in which the air enters an annular combustion chamber 20 through annular guide vanes 22, 24, retaining a considerable amount of the whirl velocity with which it leaves the compressor diffuser blades 18, but with the meridional velocity reduced below the flame propagation velocity. A series of fuel nozzles 26 are arranged in a circle about the axis of the plant. Cooling air flows between the wall of the combustion chamber and sheet metal linings 30, 42. In the embodiment shown in Fig. 5, the air passes over heat-exchanger tubes 88 before entering the annular combustion chamber 98 by way of pre-whirl vanes 90 and perforated annular guide vanes 92, 94. Fuel is injected through nozzles 96. Cooling air flows between the wall of the combustion chamber and sheet metal linings 102, 108.
GB2421954A 1954-08-19 1954-08-19 Improvements in or relating to gas turbine power plants Expired GB791232A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2421954A GB791232A (en) 1954-08-19 1954-08-19 Improvements in or relating to gas turbine power plants

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US108975A US2709893A (en) 1949-08-06 1949-08-06 Gas turbine power plant with heat exchanger and cooling means
GB2421954A GB791232A (en) 1954-08-19 1954-08-19 Improvements in or relating to gas turbine power plants
FR1111569D FR1111569A (en) 1954-08-19 1954-08-28 gas turbine plant
DEL20057A DE1130646B (en) 1954-08-19 1954-10-01 Diagonal gas turbine power plant

Publications (1)

Publication Number Publication Date
GB791232A true GB791232A (en) 1958-02-26

Family

ID=10208261

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2421954A Expired GB791232A (en) 1954-08-19 1954-08-19 Improvements in or relating to gas turbine power plants

Country Status (4)

Country Link
US (1) US2709893A (en)
DE (1) DE1130646B (en)
FR (1) FR1111569A (en)
GB (1) GB791232A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2533977A1 (en) * 1982-09-30 1984-04-06 Gen Electric Multi-stage centrifugal wheel
EP0568748A1 (en) * 1992-04-22 1993-11-10 Dae Sung Lee Heat recovering thrust turbine having rotational flow path

Families Citing this family (51)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2925714A (en) * 1954-10-11 1960-02-23 Thompson Ramo Wooldridge Inc Diffuser-regenerator gas turbine engine
GB805195A (en) * 1955-12-08 1958-12-03 Rolls Royce Improvements in or relating to gas turbine power plant
US2971339A (en) * 1956-08-23 1961-02-14 Gold Harold Gas turbine control system
US2904307A (en) * 1956-10-01 1959-09-15 Crane Co Cooling turbine
DE1033966B (en) * 1956-11-21 1958-07-10 Kloeckner Humboldt Deutz Ag Injection internal combustion engine
US3010281A (en) * 1957-12-24 1961-11-28 Adolph J Cervenka Toroidal combustion chamber
US2939626A (en) * 1957-12-27 1960-06-07 Laval Steam Turbine Co Turbo-compressor
US3030005A (en) * 1958-01-21 1962-04-17 Bertin & Cie Ejectors or jet apparatus
US2975959A (en) * 1958-09-30 1961-03-21 Berry W Foster Back-to-back centrifugal compressor and centripetal turbine having an integral rotordisc
DE1092730B (en) * 1959-02-11 1960-11-10 Daimler Benz Ag Gehaeuseausbildung for gas turbine engines
DE1278794B (en) * 1960-11-04 1968-09-26 Rudolph Birmann Verpuffungsgasturbinenanlage
DE1218800B (en) * 1961-04-25 1966-06-08 M A N Turbo Ges Mit Beschraenk Gas turbine, in particular small gas turbine
GB970188A (en) * 1963-01-31 1964-09-16 Rolls Royce Gas turbine vertical lift engine
GB970189A (en) * 1963-01-31 1964-09-16 Rolls Royce Combustion equipment for a gas turbine engine
US3232580A (en) * 1963-07-18 1966-02-01 Birmann Rudolph Centripetal turbine
DE1269418B (en) * 1964-08-21 1968-05-30 Gen Motors Corp gas turbine
US3309866A (en) * 1965-03-11 1967-03-21 Gen Electric Combustion process and apparatus
US3365892A (en) * 1965-08-10 1968-01-30 Derderian George Turbomachine
DE1301634B (en) * 1965-09-29 1969-08-21 Curtiss Wright Corp Gas turbine engine
US3493169A (en) * 1968-06-03 1970-02-03 United Aircraft Corp Bleed for compressor
US3994630A (en) * 1974-08-21 1976-11-30 International Harvester Company Monorotor turbine and method of cooling
US3995432A (en) * 1975-07-28 1976-12-07 United Technologies Corporation Collector
US4303377A (en) * 1978-02-03 1981-12-01 Schwartzman Everett H Turbine-compressor ejector
US4357796A (en) * 1980-09-30 1982-11-09 The United States Of America As Represented By The Secretary Of The Air Force Small gas turbofan engine with regenerating diffuser
US4382359A (en) * 1981-01-27 1983-05-10 Sampayo Eduardo A Gas turbine engine
DE3339505A1 (en) * 1983-10-31 1985-05-09 Bernd Jung Gas turbine with turbocompressor connected on the inlet side
EP0227638B1 (en) * 1984-01-07 1990-11-07 ROLLS-ROYCE plc Improvements in or relating to gas turbine power plant
JPH0245476Y2 (en) * 1984-09-03 1990-12-03
EP0206683A3 (en) * 1985-06-17 1988-08-03 University Of Dayton Internal bypass gas turbine engines with blade cooling
US4800717A (en) * 1986-12-22 1989-01-31 Sundstrand Corporation Turbine rotor cooling
DE3815679C2 (en) * 1988-05-07 1992-01-02 Aktiengesellschaft Kuehnle, Kopp & Kausch, 6710 Frankenthal, De
US4991390A (en) * 1988-09-26 1991-02-12 Sundstrand Corporation Mounting and cooling turbine nozzle vanes
US5101620A (en) * 1988-12-28 1992-04-07 Sundstrand Corporation Annular combustor for a turbine engine without film cooling
US4932207A (en) * 1988-12-28 1990-06-12 Sundstrand Corporation Segmented seal plate for a turbine engine
US5280703A (en) * 1989-12-11 1994-01-25 Sundstrand Corporation Turbine nozzle cooling
US5111655A (en) * 1989-12-22 1992-05-12 Sundstrand Corporation Single wall combustor assembly
US5253472A (en) * 1990-02-28 1993-10-19 Dev Sudarshan P Small gas turbine having enhanced fuel economy
US5832715A (en) * 1990-02-28 1998-11-10 Dev; Sudarshan Paul Small gas turbine engine having enhanced fuel economy
US5526640A (en) * 1994-05-16 1996-06-18 Technical Directions, Inc. Gas turbine engine including a bearing support tube cantilevered from a turbine nozzle wall
US6585482B1 (en) * 2000-06-20 2003-07-01 General Electric Co. Methods and apparatus for delivering cooling air within gas turbines
US7043811B2 (en) * 2004-03-22 2006-05-16 General Electric Company Method of removing studs
US7251942B2 (en) * 2004-06-29 2007-08-07 Honeywell International Inc. Integrated gearless and nonlubricated auxiliary power unit
US7559745B2 (en) * 2006-03-21 2009-07-14 United Technologies Corporation Tip clearance centrifugal compressor impeller
DE102009014005A1 (en) * 2009-03-19 2010-09-23 Bosch Mahle Turbo Systems Gmbh & Co. Kg Rotating fluid flow engine for exhaust turbocharger for internal combustion engine of motor vehicle, has rotor with compressor wheel and turbine wheel, where rotor is supported around rotational axis in fluid flow engine in pivoting manner
FR2944060B1 (en) * 2009-04-06 2013-07-19 Turbomeca Secondary air system for centrifugal or mixed compressor
BR112014007147A2 (en) * 2011-12-18 2017-04-04 Villarrubia Ruiz Jonás solar collector with solar turbine or turbocharger
US10527059B2 (en) 2013-10-21 2020-01-07 Williams International Co., L.L.C. Turbomachine diffuser
GB2536878A (en) * 2015-03-23 2016-10-05 Aurelia Turbines Oy Multi-spool gas turbine arrangement
GB2536876A (en) * 2015-03-23 2016-10-05 Aurelia Turbines Oy Two-spool gas turbine arrangement
US10208628B2 (en) * 2016-03-30 2019-02-19 Honeywell International Inc. Turbine engine designs for improved fine particle separation efficiency
RU2730206C1 (en) * 2019-08-15 2020-08-19 Александр Тихонович Зыбин Compressed combustion gas-turbine internal combustion engine

Family Cites Families (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE137706C (en) *
DE346599C (en) *
US1926225A (en) * 1930-09-12 1933-09-12 Birmann Rudolph Turbo compressor
US1959703A (en) * 1932-01-26 1934-05-22 Birmann Rudolph Blading for centrifugal impellers or turbines
DE644829C (en) * 1932-11-19 1937-05-14 Siemens Ag gas turbine
US2283176A (en) * 1937-11-29 1942-05-19 Turbo Engineering Corp Elastic fluid mechanism
US2256198A (en) * 1938-05-27 1941-09-16 Ernst Heinkel Aircraft power plant
DE696062C (en) * 1938-07-10 1940-09-10 Rheinmetall Borsig Ag Turbinengehaeuse, in particular for gas turbines
CH225232A (en) * 1941-02-06 1943-01-15 Bmw Flugmotorenbau Gmbh Internally cooled turbine blade.
GB586913A (en) * 1942-04-18 1947-04-08 Turbo Engineering Corp Power plant
GB587150A (en) * 1942-04-18 1947-04-16 Turbo Engineering Corp Turbine unit
US2473356A (en) * 1942-04-18 1949-06-14 Turbo Engineering Corp Combustion gas turbine arrangement
US2407531A (en) * 1942-05-02 1946-09-10 Fed Reserve Bank Elastic fluid mechanism
GB586912A (en) * 1942-05-02 1947-04-08 Turbo Engineering Turbine system
CH239435A (en) * 1942-05-23 1945-10-15 Buechi Alfred Free overhung turbine, in particular for hot gases.
US2479777A (en) * 1943-05-22 1949-08-23 Lockheed Aircraft Corp Fuel injection means for gas turbine power plants for aircraft
US2489683A (en) * 1943-11-19 1949-11-29 Edward A Stalker Turbine
US2575682A (en) * 1944-02-14 1951-11-20 Lockheed Aircraft Corp Reaction propulsion aircraft power plant having independently rotating compressor and turbine blading stages
US2563270A (en) * 1944-02-14 1951-08-07 Lockheed Aircraft Corp Gas reaction power plant with a variable area nozzle
US2613501A (en) * 1945-06-02 1952-10-14 Lockheed Aircraft Corp Internal-combustion turbine power plant
GB659151A (en) * 1948-06-02 1951-10-17 Westinghouse Electric Int Co Improvements in or relating to gas turbine power plants
US2640319A (en) * 1949-02-12 1953-06-02 Packard Motor Car Co Cooling of gas turbines
GB680581A (en) * 1949-05-09 1952-10-08 Hermann Oestrich Means for cooling the blades of gas turbine engines
BE498667A (en) * 1949-08-27
GB699865A (en) * 1950-11-06 1953-11-18 W H Allen Sons & Company Ltd Improvements in or relating to gas turbines
FR1050722A (en) * 1951-02-15 1954-01-11 Power Jets Res & Dev Ltd Improvements to the rotors for traversees machines by a fluid, such as turbines

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2533977A1 (en) * 1982-09-30 1984-04-06 Gen Electric Multi-stage centrifugal wheel
GB2127905A (en) * 1982-09-30 1984-04-18 Gen Electric Centrifugal compressor
US4502837A (en) * 1982-09-30 1985-03-05 General Electric Company Multi stage centrifugal impeller
EP0568748A1 (en) * 1992-04-22 1993-11-10 Dae Sung Lee Heat recovering thrust turbine having rotational flow path

Also Published As

Publication number Publication date
DE1130646B (en) 1962-05-30
FR1111569A (en) 1956-03-01
US2709893A (en) 1955-06-07

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