GB621438A - Improvements relating to combustion equipment for gas-turbine-engines - Google Patents

Improvements relating to combustion equipment for gas-turbine-engines

Info

Publication number
GB621438A
GB621438A GB548847A GB548847A GB621438A GB 621438 A GB621438 A GB 621438A GB 548847 A GB548847 A GB 548847A GB 548847 A GB548847 A GB 548847A GB 621438 A GB621438 A GB 621438A
Authority
GB
United Kingdom
Prior art keywords
air
perforations
section
admitted
engines
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
GB548847A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB548847A priority Critical patent/GB621438A/en
Publication of GB621438A publication Critical patent/GB621438A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F23R3/06—Arrangement of apertures along the flame tube

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Abstract

621,438. Gas turbine combustion chambers. OULIANOFF, G. Feb. 25, 1947, No. 5488. [Class 51 (i)] The diameter of a flame tube increases at the junctions of the sections 2a, 2b, 2c and the sections are joined by flanged rings 20 which are perforated at 22. Air passing through these perforations provides a layer of cooler air against the flame tube wall. Primary air is admitted through perforations 14 in an entry end wall. Secondary air is admitted through perforations 16, 19. The outer air casing comprises a cast metal section 1a, connected to an air-inlet 5 by a spherical joint 4, and a sheet metal section 1b having a flange 9 bolted to the section 1a. The cross-section of the air duct is substantially constant, or it -may decrease from the inlet to the outlet.
GB548847A 1947-02-25 1947-02-25 Improvements relating to combustion equipment for gas-turbine-engines Expired GB621438A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB548847A GB621438A (en) 1947-02-25 1947-02-25 Improvements relating to combustion equipment for gas-turbine-engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB548847A GB621438A (en) 1947-02-25 1947-02-25 Improvements relating to combustion equipment for gas-turbine-engines

Publications (1)

Publication Number Publication Date
GB621438A true GB621438A (en) 1949-04-08

Family

ID=9797142

Family Applications (1)

Application Number Title Priority Date Filing Date
GB548847A Expired GB621438A (en) 1947-02-25 1947-02-25 Improvements relating to combustion equipment for gas-turbine-engines

Country Status (1)

Country Link
GB (1) GB621438A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2699648A (en) * 1950-10-03 1955-01-18 Gen Electric Combustor sectional liner structure with annular inlet nozzles
US2795930A (en) * 1951-12-06 1957-06-18 A V Roe Canada Ltd Joint construction for combustion chamber casings
US2807934A (en) * 1951-12-06 1957-10-01 A V Roe Canada Ltd Flame tube support for a gas turbine combustion system
US3978664A (en) * 1974-12-20 1976-09-07 United Technologies Corporation Gas turbine engine diffuser

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2699648A (en) * 1950-10-03 1955-01-18 Gen Electric Combustor sectional liner structure with annular inlet nozzles
US2795930A (en) * 1951-12-06 1957-06-18 A V Roe Canada Ltd Joint construction for combustion chamber casings
US2807934A (en) * 1951-12-06 1957-10-01 A V Roe Canada Ltd Flame tube support for a gas turbine combustion system
US3978664A (en) * 1974-12-20 1976-09-07 United Technologies Corporation Gas turbine engine diffuser

Similar Documents

Publication Publication Date Title
GB706645A (en) Metallic combustion chamber for producing hot gases, particularly motive gases for gas turbine installations
GB721126A (en) Improvements in or relating to gas burners
GB1278590A (en) Combustion chambers for gas turbine engines
GB683555A (en) Improvements in or relating to combustion chamber
GB588086A (en) Improvements relating to combustion apparatus
GB650462A (en) Improvements in or relating to combustion apparatus
GB1302218A (en)
GB1040390A (en) Gas turbine engine
GB621438A (en) Improvements relating to combustion equipment for gas-turbine-engines
GB619251A (en) Improvements relating to combustion-equipment
GB721209A (en) Combustion apparatus
GB1354333A (en) Regenerative gas turbine engines
GB836135A (en) Improvements in and relating to gas turbine plant
GB1442350A (en) Gas turbine engine combustion equipment
GB845971A (en) Improvements relating to combustion chambers for gas turbine engines
GB691876A (en) Improvements in or relating to combustion apparatus using compressed air
GB866969A (en) Gas turbine engines
GB965152A (en) Improvements in or relating to primary air control devices for gas-turbine engine combustion chambers
GB738006A (en) Improvements in or relating to gas turbine engines
GB715387A (en) Improvements in or relating to combustion chambers for gas turbines or other prime movers
GB947134A (en) Improvements in or relating to combustion chambers of gas turbines
GB586602A (en) Improvements in regenerative gas turbine plants
GB694414A (en) Improvements in or relating to internal combustion gas turbine engines
FR2345669A1 (en) Balanced flue for gas burner - with combustion air drawn through tube and exhaust products released through inner coaxial tube
GB671159A (en) An improved silencer or muffler for engine and other gas exhausts