GB588086A - Improvements relating to combustion apparatus - Google Patents

Improvements relating to combustion apparatus

Info

Publication number
GB588086A
GB588086A GB5266/43A GB526643A GB588086A GB 588086 A GB588086 A GB 588086A GB 5266/43 A GB5266/43 A GB 5266/43A GB 526643 A GB526643 A GB 526643A GB 588086 A GB588086 A GB 588086A
Authority
GB
United Kingdom
Prior art keywords
air
chamber
holes
tangentially
ducts
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
GB5266/43A
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 Ltd
Original Assignee
Power Jets 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 Power Jets Ltd filed Critical Power Jets Ltd
Priority to GB5266/43A priority Critical patent/GB588086A/en
Publication of GB588086A publication Critical patent/GB588086A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/06Arrangement of apertures along the flame tube
    • 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
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/46Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • 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
    • F23R3/42Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/54Reverse-flow combustion chambers
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies

Abstract

588,086. Gas turbines. POWER JETS, Ltd., and NATHAN, M. L. April 1, 1943, No. 5266. [Class 51 (i)] A combustion chamber 8, for continuous combustion gas turbines and other purposes, is enclosed within a shell 1 through which air from an inlet 2 passes to the chamber and has an outlet 9 leading to a turbine 6. The air is admitted to the combustion chamber through holes in its cylindrical wall. The holes at 16, 17, are provided by short nozzle-shaped passages guiding the air into the chamber tangentially. The passages at 17 are arranged oppositely to those at 16. Rings of simple holes 15, 18 are also provided. Other nozzle-shaped passages at 13 admit air tangentially through the end wall of the chamber. Several chambers are arranged circularly in the turbine plant and are interconnected by-air ducts 7. The 'shells 8 are connected by pipes 20 slidingly supported in the ducts 7.
GB5266/43A 1943-04-01 1943-04-01 Improvements relating to combustion apparatus Expired GB588086A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB5266/43A GB588086A (en) 1943-04-01 1943-04-01 Improvements relating to combustion apparatus

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB5266/43A GB588086A (en) 1943-04-01 1943-04-01 Improvements relating to combustion apparatus
BE461566A BE461566A (en) 1943-04-01 1945-11-30
BE451566A BE451566A (en) 1943-04-01 1945-11-30

Publications (1)

Publication Number Publication Date
GB588086A true GB588086A (en) 1947-05-14

Family

ID=9792853

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5266/43A Expired GB588086A (en) 1943-04-01 1943-04-01 Improvements relating to combustion apparatus

Country Status (2)

Country Link
BE (2) BE461566A (en)
GB (1) GB588086A (en)

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2553091A (en) * 1948-09-11 1951-05-15 Harold R Horning Heater
US2560223A (en) * 1948-02-04 1951-07-10 Wright Aeronautical Corp Double air-swirl baffle construction for fuel burners
US2560207A (en) * 1948-02-04 1951-07-10 Wright Aeronautical Corp Annular combustion chamber with circumferentially spaced double air-swirl burners
US2601390A (en) * 1946-11-07 1952-06-24 Westinghouse Electric Corp Combustion chamber for gas turbines with circumferentially arranged pulverized solidfuel and air nozzles
US2615300A (en) * 1946-04-08 1952-10-28 Rolls Royce Combustion chamber for gas turbines and having flame tube mounting means allowing radial and axial expansion
US2651912A (en) * 1950-10-31 1953-09-15 Gen Electric Combustor and cooling means therefor
US2654996A (en) * 1948-10-26 1953-10-13 Oerlikon Maschf Gas turbine combustion chamber
US2657531A (en) * 1948-01-22 1953-11-03 Gen Electric Wall cooling arrangement for combustion devices
US2664702A (en) * 1947-08-11 1954-01-05 Power Jets Res & Dev Ltd Cooled flame tube
US2674846A (en) * 1950-12-18 1954-04-13 Lummus Co Combustion chamber with baffle means to control secondary air
US2698050A (en) * 1949-06-10 1954-12-28 Lummus Co Combustion for liquid fuels
US2718757A (en) * 1951-01-17 1955-09-27 Lummus Co Aircraft gas turbine and jet
GB2133869A (en) * 1983-01-18 1984-08-01 Deutsche Forsch Luft Raumfahrt A starting aid device for a high pressure combustion chamber
WO1991008421A1 (en) * 1989-12-05 1991-06-13 Allied-Signal Inc. Combustion apparatus and method for a turbine engine
EP1843097A1 (en) * 2006-04-04 2007-10-10 Siemens Power Generation, Inc. Air flow conditioner for a combustor can of a gas turbine engine
FR2973479A1 (en) * 2011-03-30 2012-10-05 Snecma Revolution wall e.g. external revolution wall, for combustion chamber of turbomachine of commercial plane, has circumferential row of primary air holes whose regions are located away from plane along row of dilution holes
EP2753879A1 (en) * 2011-09-08 2014-07-16 Reformtech Heating Holding AB Burner comprising a reactor for catalytic burning

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20120305670A1 (en) * 2011-06-06 2012-12-06 General Electric Company System for conditioning flow through a combustor

Cited By (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2615300A (en) * 1946-04-08 1952-10-28 Rolls Royce Combustion chamber for gas turbines and having flame tube mounting means allowing radial and axial expansion
US2601390A (en) * 1946-11-07 1952-06-24 Westinghouse Electric Corp Combustion chamber for gas turbines with circumferentially arranged pulverized solidfuel and air nozzles
US2664702A (en) * 1947-08-11 1954-01-05 Power Jets Res & Dev Ltd Cooled flame tube
US2657531A (en) * 1948-01-22 1953-11-03 Gen Electric Wall cooling arrangement for combustion devices
US2560223A (en) * 1948-02-04 1951-07-10 Wright Aeronautical Corp Double air-swirl baffle construction for fuel burners
US2560207A (en) * 1948-02-04 1951-07-10 Wright Aeronautical Corp Annular combustion chamber with circumferentially spaced double air-swirl burners
US2553091A (en) * 1948-09-11 1951-05-15 Harold R Horning Heater
US2654996A (en) * 1948-10-26 1953-10-13 Oerlikon Maschf Gas turbine combustion chamber
US2698050A (en) * 1949-06-10 1954-12-28 Lummus Co Combustion for liquid fuels
US2651912A (en) * 1950-10-31 1953-09-15 Gen Electric Combustor and cooling means therefor
US2674846A (en) * 1950-12-18 1954-04-13 Lummus Co Combustion chamber with baffle means to control secondary air
US2718757A (en) * 1951-01-17 1955-09-27 Lummus Co Aircraft gas turbine and jet
GB2133869A (en) * 1983-01-18 1984-08-01 Deutsche Forsch Luft Raumfahrt A starting aid device for a high pressure combustion chamber
WO1991008421A1 (en) * 1989-12-05 1991-06-13 Allied-Signal Inc. Combustion apparatus and method for a turbine engine
US5109671A (en) * 1989-12-05 1992-05-05 Allied-Signal Inc. Combustion apparatus and method for a turbine engine
EP1843097A1 (en) * 2006-04-04 2007-10-10 Siemens Power Generation, Inc. Air flow conditioner for a combustor can of a gas turbine engine
US7762074B2 (en) * 2006-04-04 2010-07-27 Siemens Energy, Inc. Air flow conditioner for a combustor can of a gas turbine engine
FR2973479A1 (en) * 2011-03-30 2012-10-05 Snecma Revolution wall e.g. external revolution wall, for combustion chamber of turbomachine of commercial plane, has circumferential row of primary air holes whose regions are located away from plane along row of dilution holes
EP2753879A1 (en) * 2011-09-08 2014-07-16 Reformtech Heating Holding AB Burner comprising a reactor for catalytic burning
CN103958966A (en) * 2011-09-08 2014-07-30 加热技术改良控股有限公司 Burner comprising a reactor for catalytic burning
EP2753879A4 (en) * 2011-09-08 2015-04-29 Reformtech Heating Holding Ab Burner comprising a reactor for catalytic burning
US9618198B2 (en) 2011-09-08 2017-04-11 Reformtech Heating Holding Ab Burner comprising a reactor for catalytic burning

Also Published As

Publication number Publication date
BE451566A (en) 1945-12-31
BE461566A (en) 1945-12-31

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