GB591113A - Improvements relating to the construction and mounting of fuel burner nozzles, especially for gas turbines and like apparatus - Google Patents

Improvements relating to the construction and mounting of fuel burner nozzles, especially for gas turbines and like apparatus

Info

Publication number
GB591113A
GB591113A GB1354/45A GB135445A GB591113A GB 591113 A GB591113 A GB 591113A GB 1354/45 A GB1354/45 A GB 1354/45A GB 135445 A GB135445 A GB 135445A GB 591113 A GB591113 A GB 591113A
Authority
GB
United Kingdom
Prior art keywords
burner
fuel
flame chamber
inlet connection
divides
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
GB1354/45A
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.)
Power Jets Research and Development Ltd
Original Assignee
Power Jets Research and Development 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
Priority to NL70888D priority Critical patent/NL70888C/xx
Priority to BE462369D priority patent/BE462369A/xx
Application filed by Power Jets Research and Development Ltd filed Critical Power Jets Research and Development Ltd
Priority to GB1354/45A priority patent/GB591113A/en
Priority to CH261477D priority patent/CH261477A/en
Priority to US641145A priority patent/US2575264A/en
Priority to FR920036D priority patent/FR920036A/en
Priority to FR920038D priority patent/FR920038A/en
Publication of GB591113A publication Critical patent/GB591113A/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
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/062—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with aft fan
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/06—Fluid supply conduits to nozzles or the like
    • F01D9/065—Fluid supply or removal conduits traversing the working fluid flow, e.g. for lubrication-, cooling-, or sealing fluids
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Gas Burners (AREA)
  • Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)

Abstract

591,113. Generating combustion products under pressure. POWER JETS (RESEARCH & DEVELOPMENT), Ltd., and FEILDEN, G.B.R. Jan. 16, 1945, No. 1354. [Class 51 (i)] [Also in Groups XI and XXVI] A combustion apparatus, particularly for a gas turbine plant, in which the fuel is injected in a downstream direction into a flame chamber enclosed within an air duct, has the fuel injector burner, which supports the upstream end of the flame chamber detachably mounted on a structural member of the air duct which lies in and divides the air stream and through which pass the fuel supply connections to the burner. The flame chamber is attached to the burner by releasable locking means which allows its easy withdrawal in the axial direction. A burner 5 is mounted on the downstream edge of a structural member 7 of aerofoil form in cross-section which lies in and divides the airstream so as to be removable therefrom without disturbing the fuel supply connections. The burner, which is of the. spill controlled type, receives fuel from an inlet connection 10 through axial passages 11 each of which is fitted with a tubular liner 12. The liners 12 project from each end of the member 7 and are fitted with sealing rings 14 and 16 so as to make a fluid tight joint when the bolts attaching the inlet connection 10 and the burner 5 to the member 7 are tightened up. The burner 5 supports the upstream end of the flame chamber 4 by means of a screwed sleeve 24 engaged by a locking sleeve 25. The burner nozzle 20 is formed in a separate end plate held in position on the burner by a screwed sleeve 22. The radial passage 8 not only accommodates the fuel inlet connection but also forms a passage for cooling air for the bearings and shaft. A modification using a single duct burner is also described.
GB1354/45A 1945-01-16 1945-01-16 Improvements relating to the construction and mounting of fuel burner nozzles, especially for gas turbines and like apparatus Expired GB591113A (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
NL70888D NL70888C (en) 1945-01-16
BE462369D BE462369A (en) 1945-01-16
GB1354/45A GB591113A (en) 1945-01-16 1945-01-16 Improvements relating to the construction and mounting of fuel burner nozzles, especially for gas turbines and like apparatus
CH261477D CH261477A (en) 1945-01-16 1946-01-10 Incinerator.
US641145A US2575264A (en) 1945-01-16 1946-01-14 Construction and mounting of fuel burner nozzles, especially for gas turbines and like apparatus
FR920036D FR920036A (en) 1945-01-16 1946-01-14 Improvements to gas turbine engines or the like include a combustion apparatus
FR920038D FR920038A (en) 1945-01-16 1946-01-14 Improvements to fuel burner vehicles, in particular turbo-propellants or similar

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1354/45A GB591113A (en) 1945-01-16 1945-01-16 Improvements relating to the construction and mounting of fuel burner nozzles, especially for gas turbines and like apparatus

Publications (1)

Publication Number Publication Date
GB591113A true GB591113A (en) 1947-08-07

Family

ID=29725418

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1354/45A Expired GB591113A (en) 1945-01-16 1945-01-16 Improvements relating to the construction and mounting of fuel burner nozzles, especially for gas turbines and like apparatus

Country Status (6)

Country Link
US (1) US2575264A (en)
BE (1) BE462369A (en)
CH (1) CH261477A (en)
FR (2) FR920036A (en)
GB (1) GB591113A (en)
NL (1) NL70888C (en)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2675675A (en) * 1954-04-20 Muctlpefi combustion chamber jet
US2670600A (en) * 1947-06-17 1954-03-02 Bristol Aeroplane Co Ltd Air distribution system for flame tubes of gas turbine engines
US2697032A (en) * 1949-05-05 1954-12-14 Phillips Petroleum Co Acetylene gas producer
US2711631A (en) * 1949-06-21 1955-06-28 Hartford Nat Bank & Trust Co Gas turbine power plant
US2692478A (en) * 1951-02-24 1954-10-26 Boeing Co Turbine burner incorporating removable burner liner
US2690648A (en) * 1951-07-03 1954-10-05 Dowty Equipment Ltd Means for conducting the flow of liquid fuel for feeding burners of gas turbine engines
US3062482A (en) * 1952-08-25 1962-11-06 A V Roe Canada Ltd Gas turbine engined aircraft
FR998079A (en) * 1958-08-22 1952-01-14 Snecma Device for the entry of air into the primary zone of a turbo-machine combustion chamber
US3741483A (en) * 1971-12-10 1973-06-26 Mitsubishi Heavy Ind Ltd Combustion air supply arrangement for gas turbines
US5630319A (en) * 1995-05-12 1997-05-20 General Electric Company Dome assembly for a multiple annular combustor

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2432359A (en) * 1947-12-09 Internal-combustion turbine power
US2439273A (en) * 1948-04-06 Turbo-jet engine for aircraft
US1517422A (en) * 1922-08-05 1924-12-02 Leo G Hall Combination land and water vehicle
US1466006A (en) * 1922-09-14 1923-08-28 Trood Samuel Apparatus for producing and utilizing combustible mixture
US1950046A (en) * 1933-05-12 1934-03-06 Surface Combustion Corp Gas burner
US1995417A (en) * 1933-05-12 1935-03-26 Surface Combustion Corp Gas burner
US2072731A (en) * 1934-12-03 1937-03-02 Steam Motors Inc Oil burner
US2224472A (en) * 1938-05-02 1940-12-10 Chandler Evans Corp Pressure fed carburetor
US2360130A (en) * 1941-03-26 1944-10-10 Armstrong Siddeley Motors Ltd High-speed propulsion plant
US2422214A (en) * 1944-08-17 1947-06-17 Westinghouse Electric Corp Fuel injector mounting for combustion chambers

Also Published As

Publication number Publication date
US2575264A (en) 1951-11-13
BE462369A (en)
FR920038A (en) 1947-03-25
CH261477A (en) 1949-05-15
FR920036A (en) 1947-03-25
NL70888C (en)

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