GB637220A - Installation for control of combustion for gas turbines - Google Patents

Installation for control of combustion for gas turbines

Info

Publication number
GB637220A
GB637220A GB1258848A GB1258848A GB637220A GB 637220 A GB637220 A GB 637220A GB 1258848 A GB1258848 A GB 1258848A GB 1258848 A GB1258848 A GB 1258848A GB 637220 A GB637220 A GB 637220A
Authority
GB
United Kingdom
Prior art keywords
oil
air
injector
cylinder
whirl
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
GB1258848A
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.)
JOHN BAIN KERR
Wallsend Slipway & Engineering
Original Assignee
JOHN BAIN KERR
Wallsend Slipway & Engineering
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 JOHN BAIN KERR, Wallsend Slipway & Engineering filed Critical JOHN BAIN KERR
Priority to GB1258848A priority Critical patent/GB637220A/en
Publication of GB637220A publication Critical patent/GB637220A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
    • F23D11/36—Details, e.g. burner cooling means, noise reduction means
    • F23D11/40—Mixing tubes or chambers; Burner heads
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C7/00—Combustion apparatus characterised by arrangements for air supply
    • F23C7/02—Disposition of air supply not passing through burner
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M5/00—Casings; Linings; Walls
    • F23M5/08—Cooling thereof; Tube walls
    • F23M5/085—Cooling thereof; Tube walls using air or other gas as the cooling medium
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spray-Type Burners (AREA)

Abstract

637,220. Supplying air to liquid fuel burners. WALLSEND SLIPWAY & ENGINEERING CO., Ltd., KERR, J. B., and DOBBS, A. G. May 7, 1948, No. 12588. [Class 75 (i))] [Also in Group XII] A gas turbine combustion chamber comprises inner and outer chambers 1, 2 forming between them an annular space 3 for cooling air, a burner body 10 through which the primary air passes and a cylinder 5 through which the oil-laden primary air from the burner 12 passes which cylinder has external vanes 6 to impart whirl to secondary air entering the inner chamber 1. The inner chamber has a restriction ring or quarl 4 to increase the local velocity of the air and to deflect the air into the oil spray issuing from the nozzle 12. The vanes 6 whirl the secondary air in the opposite direction to that of the oil spray. The quantity of air passing through the cylinder 5 is controlled by a flame cone 7 operated by a draw rod 8. Oil is supplied to the injector 16 through a cock 14 having a safety device 15 to prevent unscrewing of a cap 17 and removal of the injector 16 until the oil supply is cut off. When the injector 16 is removed a balanced or manually operated flap 18 prevents high pressure air entering the engine room. The oil injector 16 is held in position by a cone piece 20 forming part of the cock 14. The combustion chamber is suitable for burning fuel oil, mixtures in which coal is held in suspension in oil, creosotes or creosote and pitch mixtures.
GB1258848A 1948-05-07 1948-05-07 Installation for control of combustion for gas turbines Expired GB637220A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1258848A GB637220A (en) 1948-05-07 1948-05-07 Installation for control of combustion for gas turbines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1258848A GB637220A (en) 1948-05-07 1948-05-07 Installation for control of combustion for gas turbines

Publications (1)

Publication Number Publication Date
GB637220A true GB637220A (en) 1950-05-17

Family

ID=10007409

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1258848A Expired GB637220A (en) 1948-05-07 1948-05-07 Installation for control of combustion for gas turbines

Country Status (1)

Country Link
GB (1) GB637220A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1113331B (en) * 1958-07-30 1961-08-31 Inst Francais Du Petrol Fuels for rockets, stato and turbo reactors based on hydrocarbons
DE1173733B (en) * 1955-03-29 1964-07-09 British Petroleum Co Process to prevent or reduce damage to gas turbines and combustion chambers for gas turbines
CN104832920A (en) * 2015-05-25 2015-08-12 珠海巴陆信息科技有限公司 Fuel oil burner and steam boiler with same

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1173733B (en) * 1955-03-29 1964-07-09 British Petroleum Co Process to prevent or reduce damage to gas turbines and combustion chambers for gas turbines
DE1113331B (en) * 1958-07-30 1961-08-31 Inst Francais Du Petrol Fuels for rockets, stato and turbo reactors based on hydrocarbons
CN104832920A (en) * 2015-05-25 2015-08-12 珠海巴陆信息科技有限公司 Fuel oil burner and steam boiler with same
CN104832920B (en) * 2015-05-25 2017-03-08 珠海巴陆信息科技有限公司 Oil burner and the steam boiler with it

Similar Documents

Publication Publication Date Title
GB721126A (en) Improvements in or relating to gas burners
GB959528A (en) Burner unit
GB509252A (en) Improvements in or relating to fluid fuel burners
GB637220A (en) Installation for control of combustion for gas turbines
GB659794A (en) Improvements in or relating to means for securing stabilised burning of fuel in fast-moving air or gas streams
GB566133A (en) Improvements in and relating to oil burners for boiler and other furnaces
GB779248A (en) Improvements in or relating to gas turbine engines
GB720666A (en) Improvements relating to corner fired furnaces
GB635450A (en) Improvements relating to combustion chambers
GB387049A (en) Improvements in or relating to the firing of boilers and the like
GB821467A (en) Improvements in or relating to the generation of steam
SU75129A1 (en) Coal Burners
GB662434A (en) Improvements in combustion systems
GB701142A (en) Improvements in or relating to combustion apparatus
GB670968A (en) Vapourizing system for a gas turbine engine
GB885376A (en) Improvements relating to burners for gaseous and other fuels
GB376739A (en) Improved process of and apparatus for burning gas
GB639468A (en) Improvements in combustion systems
GB838331A (en) Improvements in oil burners for furnaces
GB799364A (en) Pulverised fuel burners
GB665770A (en) Improvements in or relating to liquid fuel burners
GB599163A (en) Improvements in liquid fuel burners
CN2090474U (en) All-function powdered coal jet burner
GB190424372A (en) Improvements in and relating to Liquid Fuel Burners.
GB1011097A (en) Improvements relating to the production of high-velocity, high-temperature gas streams