GB724176A - Improvements in and relating to combustion turbine plants - Google Patents

Improvements in and relating to combustion turbine plants

Info

Publication number
GB724176A
GB724176A GB2144950A GB2144950A GB724176A GB 724176 A GB724176 A GB 724176A GB 2144950 A GB2144950 A GB 2144950A GB 2144950 A GB2144950 A GB 2144950A GB 724176 A GB724176 A GB 724176A
Authority
GB
United Kingdom
Prior art keywords
turbine
plant
compressors
power
driving
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
GB2144950A
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.)
CA Parsons and Co Ltd
Original Assignee
CA Parsons and Co Ltd
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 CA Parsons and Co Ltd filed Critical CA Parsons and Co Ltd
Priority to GB2144950A priority Critical patent/GB724176A/en
Publication of GB724176A publication Critical patent/GB724176A/en
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
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/107—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission
    • 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
    • F02C3/085—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 the turbine being of the radial-flow type (radial-radial)
    • 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
    • F02C7/08—Heating air supply before combustion, e.g. by exhaust gases

Abstract

724,176. Gas turbine plant; centrifugal pumps and compressors. PARSONS & CO., Ltd., C. A., and HRYNISZAK, W. Nov. 30, 1951 [Aug. 30, 1950], No. 21449/50. Classes 110 (1) and 110 (3). [Also in Groups XIII and XXVIII] In a gas turbine plant comprising a power balanced radialinward flow turbine driving a radial-outward flow compressor 3 and a useful power centripetal turbine 29 driving a centrifugal compressor 2, the turbines and compressors are of the specific type shown, the combustion chamber of the plant are disposed in a plane at right angles to the axis of the plant and an air preheater is built around the exhaust duct of the centripetal turbine. The compressors have a louvred inlet 4 provided with a filter 5 and discharge into a scroll 7 having outlets 9, 8 which terminate in an annular diffuser 10. The air preheater comprises two nests of tubes having a fluid agent, such as sodium, circulated therethrough by a centri. fugal pump 19. The turbine 29 drives the pump 19 and also a rotary filter, for cleaning the exhaust gas fed to the air pre-heater, through a quill shaft 27 and a slipping clutch 26, the power shaft being driven through an epicyclic gear train as shown. Specifications 719,775 and 724,177 are referred to.
GB2144950A 1951-11-30 1951-11-30 Improvements in and relating to combustion turbine plants Expired GB724176A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2144950A GB724176A (en) 1951-11-30 1951-11-30 Improvements in and relating to combustion turbine plants

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2144950A GB724176A (en) 1951-11-30 1951-11-30 Improvements in and relating to combustion turbine plants

Publications (1)

Publication Number Publication Date
GB724176A true GB724176A (en) 1955-02-16

Family

ID=10163132

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2144950A Expired GB724176A (en) 1951-11-30 1951-11-30 Improvements in and relating to combustion turbine plants

Country Status (1)

Country Link
GB (1) GB724176A (en)

Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2850250A (en) * 1955-04-18 1958-09-02 Bedford A Smith Turbine powered convertible aircraft
US2945349A (en) * 1957-11-12 1960-07-19 Lear Inc Miniature gas turbine
US3023577A (en) * 1955-10-24 1962-03-06 Williams Res Corp Gas turbine with heat exchanger
US3032989A (en) * 1957-11-14 1962-05-08 Saurer Ag Adolph Gas turbine power plant
US3322189A (en) * 1965-12-21 1967-05-30 Ford Motor Co Heat exchange assembly
US3465518A (en) * 1966-12-14 1969-09-09 Gen Electric Radial outflow turboshaft engine
DE2628300A1 (en) * 1975-06-24 1976-12-30 Deere & Co SINGLE SHAFT GAS TURBINE DRIVE MACHINE
EP0043554A1 (en) * 1980-07-02 1982-01-13 PRATT & WHITNEY AIRCRAFT OF CANADA LIMITED Gas turbine engine
GB2131095A (en) * 1982-11-24 1984-06-13 English Electric Co Ltd Gas turbine plant
GB2169967A (en) * 1985-01-22 1986-07-23 Piers Anthony Benedict Lee Radial flow gas turbine engines
GB2170898A (en) * 1985-02-02 1986-08-13 Klaus Knizia Method and apparatus for recovering and making available process heat
US20190249560A1 (en) * 2018-02-13 2019-08-15 Corey B. Kuhns Angular Velocity Stepping and Methods of Use in Turbomachinery

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2850250A (en) * 1955-04-18 1958-09-02 Bedford A Smith Turbine powered convertible aircraft
US3023577A (en) * 1955-10-24 1962-03-06 Williams Res Corp Gas turbine with heat exchanger
US2945349A (en) * 1957-11-12 1960-07-19 Lear Inc Miniature gas turbine
US3032989A (en) * 1957-11-14 1962-05-08 Saurer Ag Adolph Gas turbine power plant
US3322189A (en) * 1965-12-21 1967-05-30 Ford Motor Co Heat exchange assembly
US3465518A (en) * 1966-12-14 1969-09-09 Gen Electric Radial outflow turboshaft engine
DE2628300A1 (en) * 1975-06-24 1976-12-30 Deere & Co SINGLE SHAFT GAS TURBINE DRIVE MACHINE
EP0043554A1 (en) * 1980-07-02 1982-01-13 PRATT & WHITNEY AIRCRAFT OF CANADA LIMITED Gas turbine engine
GB2131095A (en) * 1982-11-24 1984-06-13 English Electric Co Ltd Gas turbine plant
GB2169967A (en) * 1985-01-22 1986-07-23 Piers Anthony Benedict Lee Radial flow gas turbine engines
GB2170898A (en) * 1985-02-02 1986-08-13 Klaus Knizia Method and apparatus for recovering and making available process heat
US20190249560A1 (en) * 2018-02-13 2019-08-15 Corey B. Kuhns Angular Velocity Stepping and Methods of Use in Turbomachinery
US10851665B2 (en) * 2018-02-13 2020-12-01 Corey B. Kuhns Angular velocity stepping and methods of use in turbomachinery

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