CH255541A - Cooled metal combustion chamber for generating heating and propellant gases. - Google Patents

Cooled metal combustion chamber for generating heating and propellant gases.

Info

Publication number
CH255541A
CH255541A CH255541DA CH255541A CH 255541 A CH255541 A CH 255541A CH 255541D A CH255541D A CH 255541DA CH 255541 A CH255541 A CH 255541A
Authority
CH
Switzerland
Prior art keywords
combustion chamber
propellant gases
cooled metal
generating heating
metal combustion
Prior art date
Application number
Other languages
German (de)
Inventor
Cie Aktiengesellschaft Boveri
Original Assignee
Bbc Brown Boveri & Cie
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 Bbc Brown Boveri & Cie filed Critical Bbc Brown Boveri & Cie
Publication of CH255541A publication Critical patent/CH255541A/en

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
    • F23R3/002—Wall structures
    • 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
    • F23R3/08—Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00—Function
    • F05B2260/20—Heat transfer, e.g. cooling
    • F05B2260/221—Improvement of heat transfer
    • F05B2260/224—Improvement of heat transfer by increasing the heat transfer surface
    • F05B2260/2241—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
  • Combustion Of Fluid Fuel (AREA)
CH255541D 1947-05-12 1947-05-12 Cooled metal combustion chamber for generating heating and propellant gases. CH255541A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH647293X 1947-05-12

Publications (1)

Publication Number Publication Date
CH255541A true CH255541A (en) 1948-06-30

Family

ID=4525864

Family Applications (1)

Application Number Title Priority Date Filing Date
CH255541D CH255541A (en) 1947-05-12 1947-05-12 Cooled metal combustion chamber for generating heating and propellant gases.

Country Status (4)

Country Link
US (1) US2617255A (en)
CH (1) CH255541A (en)
DE (1) DE863153C (en)
GB (1) GB647293A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2684572A (en) * 1949-12-12 1954-07-27 Babcock & Wilcox Co Segmental wall construction for combustion apparatus
DE942602C (en) * 1951-06-25 1956-05-03 Parsons C A & Co Ltd Gas turbine with an annular combustion chamber
DE970426C (en) * 1950-11-17 1958-09-18 Power Jets Res & Dev Ltd Cyclone combustion chamber for gas turbines
DE1059719B (en) * 1955-06-16 1959-06-18 Jan Jerie Dr Ing Cooled wall of a combustion chamber, especially for gas turbines
EP0219723A1 (en) * 1985-10-04 1987-04-29 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Annular combustion chamber for gas turbines

Families Citing this family (58)

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US2727566A (en) * 1943-03-13 1955-12-20 Claude A Bonvillian Apparatus for the combustion of fuel
GB715910A (en) * 1952-02-01 1954-09-22 Rolls Royce Improvements in or relating to combustion equipment of gas-turbine engines
US2841381A (en) * 1953-05-14 1958-07-01 Basil E Jones Tobacco curer
US2775094A (en) * 1953-12-03 1956-12-25 Gen Electric End cap for fluid fuel combustor
BE535906A (en) * 1954-02-23
US2874536A (en) * 1954-03-18 1959-02-24 Gen Electric Cooling means for tailpipe
BE535497A (en) * 1954-02-26
GB758213A (en) * 1954-03-03 1956-10-03 Parsons & Marine Eng Turbine Improvements in and relating to cylindrical combustion chambers or furnaces
DE1108372B (en) * 1956-11-01 1961-06-08 Josef Cermak Dr Ing Cooling device for thermally highly stressed walls
NL248467A (en) * 1957-02-18
DE1107872B (en) * 1958-12-02 1961-05-31 Degussa Method and device for the combustion of gases containing combustible solids with a low calorific value
US3038309A (en) * 1959-07-21 1962-06-12 Gen Electric Cooling liner for jet engine afterburner
GB1605213A (en) * 1961-10-23 1984-08-30 Rolls Royce Mixing chambers for continuous flow engines
GB1038661A (en) * 1961-12-05 1966-08-10 Ass Elect Ind Improvements relating to metallic gas turbine combustion chambers
US3185458A (en) * 1963-05-13 1965-05-25 Zink Co John Direct fired air heater
CH428324A (en) * 1964-05-21 1967-01-15 Prvni Brnenska Strojirna Combustion chamber
US3532332A (en) * 1968-09-25 1970-10-06 American Pollution Prevention Rotary dehydrator system
US3539284A (en) * 1969-03-12 1970-11-10 John J Wolfersperger Two-chamber fuel burner
US3545202A (en) * 1969-04-02 1970-12-08 United Aircraft Corp Wall structure and combustion holes for a gas turbine engine
US4392355A (en) * 1969-11-13 1983-07-12 General Motors Corporation Combustion liner
US3706203A (en) * 1970-10-30 1972-12-19 United Aircraft Corp Wall structure for a gas turbine engine
US3736747A (en) * 1971-07-09 1973-06-05 G Warren Combustor
US4555901A (en) * 1972-12-19 1985-12-03 General Electric Company Combustion chamber construction
US4480436A (en) * 1972-12-19 1984-11-06 General Electric Company Combustion chamber construction
US4912922A (en) * 1972-12-19 1990-04-03 General Electric Company Combustion chamber construction
US3956886A (en) * 1973-12-07 1976-05-18 Joseph Lucas (Industries) Limited Flame tubes for gas turbine engines
US3990231A (en) * 1974-10-24 1976-11-09 General Motors Corporation Interconnections between ceramic rings permitting relative radial movement
US4236378A (en) * 1978-03-01 1980-12-02 General Electric Company Sectoral combustor for burning low-BTU fuel gas
GB2034874A (en) * 1978-11-03 1980-06-11 Gen Electric Gas turbine engine combustor
US4292810A (en) * 1979-02-01 1981-10-06 Westinghouse Electric Corp. Gas turbine combustion chamber
US4361010A (en) * 1980-04-02 1982-11-30 United Technologies Corporation Combustor liner construction
US4302941A (en) * 1980-04-02 1981-12-01 United Technologies Corporation Combuster liner construction for gas turbine engine
US4414816A (en) * 1980-04-02 1983-11-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Combustor liner construction
US4845940A (en) * 1981-02-27 1989-07-11 Westinghouse Electric Corp. Low NOx rich-lean combustor especially useful in gas turbines
US4419863A (en) * 1981-09-30 1983-12-13 United Technologies Corporation Fuel-air mixing apparatus
US4773227A (en) * 1982-04-07 1988-09-27 United Technologies Corporation Combustion chamber with improved liner construction
DE3230379C2 (en) * 1982-05-10 1987-03-26 W + E Umwelttechnik AG, Zürich Device for burning garbage and other waste in a combustion chamber
US5653110A (en) * 1991-07-22 1997-08-05 General Electric Company Film cooling of jet engine components
JP2597800B2 (en) * 1992-06-12 1997-04-09 ゼネラル・エレクトリック・カンパニイ Gas turbine engine combustor
US5327727A (en) * 1993-04-05 1994-07-12 General Electric Company Micro-grooved heat transfer combustor wall
US5337568A (en) * 1993-04-05 1994-08-16 General Electric Company Micro-grooved heat transfer wall
DE19641957A1 (en) * 1996-10-11 1998-04-16 Abb Research Ltd Device for sealing combustion chamber bricks
CA2288557C (en) * 1998-11-12 2007-02-06 Mitsubishi Heavy Industries, Ltd. Gas turbine combustor cooling structure
US20020066273A1 (en) * 2000-12-04 2002-06-06 Mitsubishi Heavy Industries, Ltd. Plate fin and combustor using the plate fin
EP1413831A1 (en) * 2002-10-21 2004-04-28 Siemens Aktiengesellschaft Annular combustor for a gas turbine and gas turbine
GB2453946B (en) * 2007-10-23 2010-07-14 Rolls Royce Plc A Wall Element for use in Combustion Apparatus
DE102007050664A1 (en) * 2007-10-24 2009-04-30 Man Turbo Ag Burner for a turbomachine, baffle for such a burner and a turbomachine with such a burner
GB0800294D0 (en) * 2008-01-09 2008-02-20 Rolls Royce Plc Gas heater
GB0801839D0 (en) * 2008-02-01 2008-03-05 Rolls Royce Plc combustion apparatus
GB2457281B (en) * 2008-02-11 2010-09-08 Rolls Royce Plc A Combustor Wall Arrangement with Parts Joined by Mechanical Fasteners
GB0803366D0 (en) * 2008-02-26 2008-04-02 Rolls Royce Plc Nose cone assembly
GB2460634B (en) * 2008-06-02 2010-07-07 Rolls Royce Plc Combustion apparatus
US8622737B2 (en) * 2008-07-16 2014-01-07 Robert S. Babington Perforated flame tube for a liquid fuel burner
US8402764B1 (en) * 2009-09-21 2013-03-26 Florida Turbine Technologies, Inc. Transition duct with spiral cooling channels
US8307654B1 (en) * 2009-09-21 2012-11-13 Florida Turbine Technologies, Inc. Transition duct with spiral finned cooling passage
US8955330B2 (en) * 2011-03-29 2015-02-17 Siemens Energy, Inc. Turbine combustion system liner
CN105318356A (en) * 2014-07-21 2016-02-10 北京航天动力研究所 High aspect ratio variable section heat exchange channel
US11506384B2 (en) 2019-02-22 2022-11-22 Dyc Turbines Free-vortex combustor

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1440095A (en) * 1919-11-14 1922-12-26 Charles D Mosher Fuel-burning apparatus
US2268464A (en) * 1939-09-29 1941-12-30 Bbc Brown Boveri & Cie Combustion chamber
GB597151A (en) * 1943-03-13 1948-01-20 Claude Albert Bonvillian Improvements in apparatus for the combustion of fuel
US2464791A (en) * 1943-11-05 1949-03-22 Claude A Bonvillian Apparatus for the combustion of fuel
US2458066A (en) * 1944-07-20 1949-01-04 American Locomotive Co Combustion chamber
BE489359A (en) * 1944-10-05
US2476031A (en) * 1944-12-02 1949-07-12 American Locomotive Co Reheater
US2493641A (en) * 1946-06-18 1950-01-03 Westinghouse Electric Corp Turbine apparatus
US2491434A (en) * 1947-04-25 1949-12-13 Bituminous Coal Research Combination power plant and heating system

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2684572A (en) * 1949-12-12 1954-07-27 Babcock & Wilcox Co Segmental wall construction for combustion apparatus
DE970426C (en) * 1950-11-17 1958-09-18 Power Jets Res & Dev Ltd Cyclone combustion chamber for gas turbines
DE942602C (en) * 1951-06-25 1956-05-03 Parsons C A & Co Ltd Gas turbine with an annular combustion chamber
DE1059719B (en) * 1955-06-16 1959-06-18 Jan Jerie Dr Ing Cooled wall of a combustion chamber, especially for gas turbines
EP0219723A1 (en) * 1985-10-04 1987-04-29 Mtu Motoren- Und Turbinen-Union MàœNchen Gmbh Annular combustion chamber for gas turbines

Also Published As

Publication number Publication date
GB647293A (en) 1950-12-13
US2617255A (en) 1952-11-11
DE863153C (en) 1953-01-15

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