GB686383A - Improvements in or relating to gas-turbine engines - Google Patents

Improvements in or relating to gas-turbine engines

Info

Publication number
GB686383A
GB686383A GB1702849A GB1702849A GB686383A GB 686383 A GB686383 A GB 686383A GB 1702849 A GB1702849 A GB 1702849A GB 1702849 A GB1702849 A GB 1702849A GB 686383 A GB686383 A GB 686383A
Authority
GB
United Kingdom
Prior art keywords
flame tube
air
duct part
annular
air casing
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
GB1702849A
Inventor
George Oulianoff
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Priority to GB1702849A priority Critical patent/GB686383A/en
Publication of GB686383A publication Critical patent/GB686383A/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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting means
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/283—Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)

Abstract

686,383. Generating combustion products under pressure. ROLLS-ROYCE, Ltd. June 9, 1950 [June 27, 1949], No. 17028/49. Class 51 (i). In an air-jacketed type of combustion chamber for gas turbine engines, the air entering the inlet end of the flame tube is separated from that flowing around the outside of the flame tube by means comprising a duct part made in one piece of which one edge divides the air flow and which is supported from the wall of the expansion chamber portion of the air casing by one or more struts, the outlet end of the duct part also supporting the inlet end of the flame tube. In the case of combustion equipment of the type comprising a flame tube mounted in an individual air casing, or of the type comprising a plurality of flame tubes in an annular air casing, the duct part 15 is of frusto-conical form and is supported by three struts 16 from the wall of the expansion chamber 10a and the mouth of the flame tube 11 is supported on the cylindrical seat 23 formed on the duct part, the radial wall 24 being provided to limit axial movement of the flame tube. The struts 16 are extended at 16a and form a boss 19 on which is mounted a fuel injector 20, ducts 21 being formed in the strut for the flow of oil from the union plug 22. In the case of combustion equipment of the type comprising an annular flame tube in an annular air casing, Fig. 7, the means for dividing the air into the two streams comprises an annular duct 58 of divergent cross-section formed of a number of duct parts, the cross-section of each of which is a sector of an annulus. Each duct part has an integral strut 59 which is connected to the outer wall of the air casing and the radially inner and outer walls of each duct part have axial flanges which together provide annular seats to support the inner and outer walls of the flame tube. The inner and outer walls of the air casing are connected by radial webs 65 on which are formed axially-extending bosses 66 which carry at their downstream ends, fuel injection devices 67. Specification 686,382 is referred to.
GB1702849A 1949-06-27 1949-06-27 Improvements in or relating to gas-turbine engines Expired GB686383A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1702849A GB686383A (en) 1949-06-27 1949-06-27 Improvements in or relating to gas-turbine engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1702849A GB686383A (en) 1949-06-27 1949-06-27 Improvements in or relating to gas-turbine engines

Publications (1)

Publication Number Publication Date
GB686383A true GB686383A (en) 1953-01-21

Family

ID=10087916

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1702849A Expired GB686383A (en) 1949-06-27 1949-06-27 Improvements in or relating to gas-turbine engines

Country Status (1)

Country Link
GB (1) GB686383A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1055884B (en) * 1954-03-02 1959-04-23 Bristol Aero Engines Ltd Flame tube for a combustion chamber of a gas turbine engine
US3303644A (en) * 1963-12-04 1967-02-14 Rolls Royce Combustion equipment for a gas turbine engine
EP1548362A1 (en) * 2003-12-25 2005-06-29 Kawasaki Jukogyo Kabushiki Kaisha Fuel supply method and fuel supply system for fuel injection device

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1055884B (en) * 1954-03-02 1959-04-23 Bristol Aero Engines Ltd Flame tube for a combustion chamber of a gas turbine engine
US3303644A (en) * 1963-12-04 1967-02-14 Rolls Royce Combustion equipment for a gas turbine engine
EP1548362A1 (en) * 2003-12-25 2005-06-29 Kawasaki Jukogyo Kabushiki Kaisha Fuel supply method and fuel supply system for fuel injection device
US7225996B2 (en) 2003-12-25 2007-06-05 Kawasaki Jukogyo Kabushiki Kaisha Fuel supply method and fuel supply system for fuel injection device

Similar Documents

Publication Publication Date Title
GB1427146A (en) Combustion apparatus for gas turbine engines
GB790293A (en) Improvements in or relating to heat-resisting wall structures for gas-turbine enginecombustion equipment
GB665247A (en) Improvements in or relating to combustion apparatus
GB780493A (en) Improvements relating to combustion equipment for gas-turbine engines
GB894470A (en) Improvements in flame tubes for burning liquid fuel in an air stream
GB1075958A (en) Gas turbine engine
GB1180524A (en) Gas Turbine Jet Engine of the By-Pass Type
US2632299A (en) Precombustion chamber
GB884756A (en) Primary air intake device for the combustion chamber of a gas-turbine unit
GB894054A (en) Improvements in or relating to combustion chambers for use in gas turbine installations
GB1132940A (en) Annular combustion equipment for a gas turbine engine
GB871842A (en) Improvements in or relating to gas turbine engines
GB1180929A (en) Combustion Apparatus, for example for Gas Turbines.
GB812201A (en) Improvements in combustion equipment for continuous-flow internal combustion engines
GB686383A (en) Improvements in or relating to gas-turbine engines
GB824306A (en) Improvements in or relating to combustion equipment of gas-turbine engines
GB694448A (en) Improvements in or relating to gas-turbine engines
GB798865A (en) Improvements in and relating to combustion systems for axial-flow gas turbine engines and ram jet engines
GB887829A (en) Improvements relating to flame tubes for combustion systems
GB710353A (en) Improvements in or relating to combustion equipment for gas-turbine engines
GB719301A (en) Improvements relating to gas turbine engines
GB744593A (en) Improvements in or relating to combustion equipment of gas turbine engines
GB670092A (en) Improvements relating to combustion equipment for gas-turbine engines
GB694484A (en) Improvements relating to combustion equipment for gas turbine engines
GB1196168A (en) Combustion Assemblies for Gas-Turbine Engines