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GB749267A - Improvements relating to open-cycle gas-turbine plant - Google Patents

Improvements relating to open-cycle gas-turbine plant

Info

Publication number
GB749267A
GB749267A GB2602253A GB2602253A GB749267A GB 749267 A GB749267 A GB 749267A GB 2602253 A GB2602253 A GB 2602253A GB 2602253 A GB2602253 A GB 2602253A GB 749267 A GB749267 A GB 749267A
Authority
GB
United Kingdom
Prior art keywords
combustion chamber
turbine plant
open
pressure
turbine
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
GB2602253A
Inventor
David Macleish Smith
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.)
Metropolitan Vickers Electrical Co Ltd
Original Assignee
Metropolitan Vickers Electrical 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 Metropolitan Vickers Electrical Co Ltd filed Critical Metropolitan Vickers Electrical Co Ltd
Priority to GB2602253A priority Critical patent/GB749267A/en
Publication of GB749267A publication Critical patent/GB749267A/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
    • F02C3/36Open cycles
    • F02C3/365Open cycles a part of the compressed air being burned, the other part being heated indirectly
    • 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
    • F02C6/00Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/003Gas-turbine plants with heaters between turbine stages
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/005Combined with pressure or heat exchangers
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/20Heat transfer, e.g. cooling
    • F05D2260/205Cooling fluid recirculation, i.e. after cooling one or more components is the cooling fluid recovered and used elsewhere for other purposes

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)

Abstract

749,267. Gas turbine plant. METROPOLITAN-VICKERS ELECTRICAL CO., Ltd. June 10, 1954 [Sept. 21, 1953], No. 26022/53. Class 110(3) In an open-circuit gas turbine plant of the kind in which high-pressure air from one or more compressors 2, 4 is supplied to at least one main combustion chamber 6, which supplies combustion products to a high-pressure turbine 9 a re-heat combustion chamber 10 being provided ahead of a low-pressure turbine 12, high pressure air is bled at 16 from the supply to the main combustion chamber 6 and used to cool a part or parts of the reheat combustion chamber 10 and is returned to the main stream at a point 20 downstream of the main combustion chamber 6 and preferably before the turbine 9. The cooling air is circulated at 18 through suitable passages or cavities within or in thermal relation to the parts to be cooled. The circulation is effected by the pressure difference between the points 16 and 20. An intercooler 3 and a preheater 5 are provided.
GB2602253A 1953-09-21 1953-09-21 Improvements relating to open-cycle gas-turbine plant Expired GB749267A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2602253A GB749267A (en) 1953-09-21 1953-09-21 Improvements relating to open-cycle gas-turbine plant

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2602253A GB749267A (en) 1953-09-21 1953-09-21 Improvements relating to open-cycle gas-turbine plant

Publications (1)

Publication Number Publication Date
GB749267A true GB749267A (en) 1956-05-23

Family

ID=10237134

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2602253A Expired GB749267A (en) 1953-09-21 1953-09-21 Improvements relating to open-cycle gas-turbine plant

Country Status (1)

Country Link
GB (1) GB749267A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3765170A (en) * 1970-12-27 1973-10-16 Toyota Motor Co Ltd Composite gas turbine set
WO1999045251A1 (en) * 1998-03-04 1999-09-10 Solo Energy Corporation Multi-shaft reheat turbine
US6107693A (en) * 1997-09-19 2000-08-22 Solo Energy Corporation Self-contained energy center for producing mechanical, electrical, and heat energy

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3765170A (en) * 1970-12-27 1973-10-16 Toyota Motor Co Ltd Composite gas turbine set
US6107693A (en) * 1997-09-19 2000-08-22 Solo Energy Corporation Self-contained energy center for producing mechanical, electrical, and heat energy
US6313544B1 (en) 1997-09-19 2001-11-06 Solo Energy Corporation Self-contained energy center for producing mechanical, electrical, and heat energy
WO1999045251A1 (en) * 1998-03-04 1999-09-10 Solo Energy Corporation Multi-shaft reheat turbine

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