GB985907A - Improvements in and relating to gas turbines - Google Patents

Improvements in and relating to gas turbines

Info

Publication number
GB985907A
GB985907A GB1087163A GB1087163A GB985907A GB 985907 A GB985907 A GB 985907A GB 1087163 A GB1087163 A GB 1087163A GB 1087163 A GB1087163 A GB 1087163A GB 985907 A GB985907 A GB 985907A
Authority
GB
United Kingdom
Prior art keywords
turbine
compressor
gases
combustion chamber
disposed around
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
GB1087163A
Inventor
George Tabberer
Vivian Archibald Hyett
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.)
Associated Electrical Industries Ltd
Original Assignee
Associated Electrical Industries 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 Associated Electrical Industries Ltd filed Critical Associated Electrical Industries Ltd
Priority to GB1087163A priority Critical patent/GB985907A/en
Publication of GB985907A publication Critical patent/GB985907A/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
    • 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
    • F02C7/26—Starting; Ignition
    • F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/275—Mechanical drives
    • F02C7/277—Mechanical drives the starter being a separate turbine
    • 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
    • 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
    • F02C3/10—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor
    • F02C3/103—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor the compressor being of the centrifugal type
    • 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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/003—Gas-turbine plants with heaters between turbine stages

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)

Abstract

985,907. Gas turbine engines. ASSOCIATED ELECTRICAL INDUSTRIES Ltd. March 5, 1964 [March 19, 1963], No. 10871/63. Heading FIG. A gas turbine engine comprises a compressor, a first combustion chamber disposed around the compressor, a first turbine which drives the compressor, a second turbine which provides useful power, the gases from the first turbine passing to a second combustion chamber disposed around the second turbine wherein the gases are reheated before passing to the second turbine. The engine shown comprises a centrifugal compressor 1 and a first turbine 2 disposed back-toback, air from the compressor passing through duct 5 into the first combustion chamber 4 which is disposed around the compressor. Gases from the combustion chamber pass through inlet 6 to drive the turbine 2 which in turn drives the compressor, the gases then passing through ducts 13, 12 to a second combustion chamber which is disposed around a second turbine 10 which provides useful power. The gases are reheated in the second chamber and then pass to the second turbine. The inlet ducts 5 and 12 are separated from the respective combustion chambers by means of baffles 7 and 14. The engine may be used as an engine starter.
GB1087163A 1963-03-19 1963-03-19 Improvements in and relating to gas turbines Expired GB985907A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1087163A GB985907A (en) 1963-03-19 1963-03-19 Improvements in and relating to gas turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1087163A GB985907A (en) 1963-03-19 1963-03-19 Improvements in and relating to gas turbines

Publications (1)

Publication Number Publication Date
GB985907A true GB985907A (en) 1965-03-10

Family

ID=9975859

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1087163A Expired GB985907A (en) 1963-03-19 1963-03-19 Improvements in and relating to gas turbines

Country Status (1)

Country Link
GB (1) GB985907A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2288640A (en) * 1994-04-16 1995-10-25 Rolls Royce Plc Gas turbine engine combustion arrangement
GB2307008A (en) * 1995-11-13 1997-05-14 Fred Moseley Gas turbine engine with two stage combustion

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2288640A (en) * 1994-04-16 1995-10-25 Rolls Royce Plc Gas turbine engine combustion arrangement
US5743081A (en) * 1994-04-16 1998-04-28 Rolls-Royce Plc Gas turbine engine
GB2288640B (en) * 1994-04-16 1998-08-12 Rolls Royce Plc A gas turbine engine
GB2307008A (en) * 1995-11-13 1997-05-14 Fred Moseley Gas turbine engine with two stage combustion

Similar Documents

Publication Publication Date Title
GB497188A (en) An internal combustion engine for use at high altitudes charged by turbo-blowers
GB905136A (en) Improvements relating to gas turbine power units
GB588096A (en) Improvements in or relating to internal combustion turbine power plants
GB774425A (en) Improvements in or relating to turbine engines
GB1229007A (en)
GB586570A (en) Improvements in internal combustion turbine plant for propulsion
GB990914A (en) Improved method and apparatus for producing working gas for heat engines
GB1093682A (en) Improvements in or relating to power plants
GB985907A (en) Improvements in and relating to gas turbines
GB585763A (en) Improvements relating to combustion chambers
GB705611A (en) Improved gas turbine power plant
GB436709A (en) Improvements in internal combustion turbines
GB529786A (en) Improvements in or relating to gas turbine installations
GB588097A (en) Improvements in or relating to internal combustion turbine power plants
GB268861A (en) Improvements in systems of gas turbine aggregates
GB683589A (en) Improvements in or relating to power plants including an internal combustion engine and an exhaust-driven turbine
GB600608A (en) Improvements in or relating to internal combustion turbine power plants
GB992931A (en) Gas turbine jet propulsion engine
GB585398A (en) Combustion chamber unit
GB1077583A (en) Improvements relating to gas turbines with pulsating gas flows
GB511331A (en) Internal combustion turbine
GB1392122A (en) Fluid flow turbomachinery
GB730383A (en) Improvements in or relating to gas turbines
GB813990A (en) Improvements in gas turbines utilising the waste heat of internal combustion engines
GB1084416A (en) Gas turbine installation