CH265007A - Verbrennungseinrichtung für Gasturbinenanlagen. - Google Patents

Verbrennungseinrichtung für Gasturbinenanlagen.

Info

Publication number
CH265007A
CH265007A CH265007DA CH265007A CH 265007 A CH265007 A CH 265007A CH 265007D A CH265007D A CH 265007DA CH 265007 A CH265007 A CH 265007A
Authority
CH
Switzerland
Prior art keywords
gas turbine
combustion device
turbine plants
plants
combustion
Prior art date
Application number
Other languages
English (en)
Inventor
Corporation Westingho Electric
Original Assignee
Westinghouse Electric Corp
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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Publication of CH265007A publication Critical patent/CH265007A/de

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
    • 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
    • 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
    • F23R3/46—Combustion chambers comprising an annular arrangement of several essentially tubular flame tubes within a common annular casing or within individual casings
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
CH265007D 1943-11-23 1947-06-26 Verbrennungseinrichtung für Gasturbinenanlagen. CH265007A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US511468A US2595999A (en) 1943-11-23 1943-11-23 Power plant combustion apparatus having apertured combustion chamber walls

Publications (1)

Publication Number Publication Date
CH265007A true CH265007A (de) 1949-11-15

Family

ID=24035037

Family Applications (1)

Application Number Title Priority Date Filing Date
CH265007D CH265007A (de) 1943-11-23 1947-06-26 Verbrennungseinrichtung für Gasturbinenanlagen.

Country Status (5)

Country Link
US (1) US2595999A (de)
CH (1) CH265007A (de)
DE (1) DE833741C (de)
FR (1) FR944726A (de)
GB (1) GB592505A (de)

Families Citing this family (46)

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NL78931C (de) * 1944-03-16
US2885858A (en) * 1947-12-02 1959-05-12 Power Jets Res & Dev Ltd Combustion system with mixing chamber
US2696076A (en) * 1949-11-28 1954-12-07 Ivan F Weeks Turbulence and combustion-promoting device for ram jet motors
US2651912A (en) * 1950-10-31 1953-09-15 Gen Electric Combustor and cooling means therefor
US2711072A (en) * 1951-06-14 1955-06-21 Gen Motors Corp Combustion chamber fairing
US2800767A (en) * 1952-12-31 1957-07-30 United Aircraft Corp Combustion section construction
US2836379A (en) * 1954-05-18 1958-05-27 Gen Dyanmics Corp Ramjet wing system for jet propelled aircraft
US2944398A (en) * 1954-10-20 1960-07-12 Lockheed Aircraft Corp Combustion chamber for jet propulsion motors
US2944388A (en) * 1955-02-24 1960-07-12 Thompson Ramo Wooldridge Inc Air atomizing spray bar
US3037351A (en) * 1956-05-14 1962-06-05 Paul O Tobeler Combustion turbine
US2988139A (en) * 1956-11-14 1961-06-13 Sebac Nouvelie S A Spraying device
US2974485A (en) * 1958-06-02 1961-03-14 Gen Electric Combustor for fluid fuels
US3051464A (en) * 1958-10-20 1962-08-28 Maxon Premix Burner Company Air-heating gas burner
US4044683A (en) * 1959-08-20 1977-08-30 Mcdonnell Douglas Corporation Heat generator
US3064720A (en) * 1960-10-18 1962-11-20 Eclipse Fuel Eng Co Burner construction
US3145533A (en) * 1962-07-13 1964-08-25 Ollinger George Batchelder Jet-thrust internal combustion engine
US3242670A (en) * 1962-08-27 1966-03-29 United Aircraft Corp Segmented baffle injector design
US3223142A (en) * 1962-11-19 1965-12-14 James A Harrison Automatic gas burner with variable flame port area
US3178161A (en) * 1963-03-05 1965-04-13 Maxon Premix Burner Company In Air heating gas burner
US3186697A (en) * 1964-12-23 1965-06-01 Mid Continent Metal Products C Gas-fired heater
GB1073335A (en) * 1965-06-21 1967-06-21 Rolls Royce Gas turbine engine combustion chamber
US4194358A (en) * 1977-12-15 1980-03-25 General Electric Company Double annular combustor configuration
US4475344A (en) * 1982-02-16 1984-10-09 Westinghouse Electric Corp. Low smoke combustor for land based combustion turbines
US4991398A (en) * 1989-01-12 1991-02-12 United Technologies Corporation Combustor fuel nozzle arrangement
US5118284A (en) * 1991-02-04 1992-06-02 Engineered Air Systems Combustion apparatus for fluid fuels and method of combusting fuel-air mixtures
US6192689B1 (en) * 1998-03-18 2001-02-27 General Electric Company Reduced emissions gas turbine combustor
US7874138B2 (en) * 2008-09-11 2011-01-25 Siemens Energy, Inc. Segmented annular combustor
TWI435978B (zh) * 2011-10-31 2014-05-01 Atomic Energy Council 富氫氣體燃燒器
US11428413B2 (en) 2016-03-25 2022-08-30 General Electric Company Fuel injection module for segmented annular combustion system
US10520194B2 (en) 2016-03-25 2019-12-31 General Electric Company Radially stacked fuel injection module for a segmented annular combustion system
US10830442B2 (en) 2016-03-25 2020-11-10 General Electric Company Segmented annular combustion system with dual fuel capability
US10641176B2 (en) 2016-03-25 2020-05-05 General Electric Company Combustion system with panel fuel injector
US10584876B2 (en) 2016-03-25 2020-03-10 General Electric Company Micro-channel cooling of integrated combustor nozzle of a segmented annular combustion system
US10563869B2 (en) 2016-03-25 2020-02-18 General Electric Company Operation and turndown of a segmented annular combustion system
US10641491B2 (en) 2016-03-25 2020-05-05 General Electric Company Cooling of integrated combustor nozzle of segmented annular combustion system
US10584880B2 (en) 2016-03-25 2020-03-10 General Electric Company Mounting of integrated combustor nozzles in a segmented annular combustion system
US10605459B2 (en) 2016-03-25 2020-03-31 General Electric Company Integrated combustor nozzle for a segmented annular combustion system
US11156362B2 (en) 2016-11-28 2021-10-26 General Electric Company Combustor with axially staged fuel injection
US10690350B2 (en) 2016-11-28 2020-06-23 General Electric Company Combustor with axially staged fuel injection
US11994292B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus for turbomachine
US11371702B2 (en) 2020-08-31 2022-06-28 General Electric Company Impingement panel for a turbomachine
US11460191B2 (en) 2020-08-31 2022-10-04 General Electric Company Cooling insert for a turbomachine
US11614233B2 (en) 2020-08-31 2023-03-28 General Electric Company Impingement panel support structure and method of manufacture
US11994293B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus support structure and method of manufacture
US11255545B1 (en) 2020-10-26 2022-02-22 General Electric Company Integrated combustion nozzle having a unified head end
US11767766B1 (en) 2022-07-29 2023-09-26 General Electric Company Turbomachine airfoil having impingement cooling passages

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US515422A (en) * 1894-02-27 chandleb
US2405723A (en) * 1946-08-13 Propulsion apparatus
US635919A (en) * 1895-06-24 1899-10-31 Charles G Curtis Apparatus for generating mechanical power.
US812513A (en) * 1905-02-27 1906-02-13 Luigi Moreno Apparatus for burning gas.
FR497772A (fr) * 1919-04-02 1919-12-17 Georges Henri Marius Canton Chambre de combustion pour moteur à combustion externe ou pour rechauffage d'air comprimé par combustion interne
FR542528A (fr) * 1921-10-18 1922-08-16 Moteur à combustion interne
US1542326A (en) * 1923-12-03 1925-06-16 Sawyer George Oil burner
US1837763A (en) * 1928-09-14 1931-12-22 Lancey Ralph W De Oil burner
US1923614A (en) * 1931-04-06 1933-08-22 Clarkson Thomas Burner control system
US2072731A (en) * 1934-12-03 1937-03-02 Steam Motors Inc Oil burner
CH210655A (de) * 1938-09-16 1940-07-31 Sulzer Ag Axial arbeitende Brennkraftturbine.
US2326072A (en) * 1939-06-28 1943-08-03 Bbc Brown Boveri & Cie Gas turbine plant
US2268464A (en) * 1939-09-29 1941-12-30 Bbc Brown Boveri & Cie Combustion chamber
US2225775A (en) * 1940-01-26 1940-12-24 David L Garrett Apparatus for deparaffining oil wells
US2360130A (en) * 1941-03-26 1944-10-10 Armstrong Siddeley Motors Ltd High-speed propulsion plant
US2409177A (en) * 1942-04-01 1946-10-15 Allis Chalmers Mfg Co Jet propulsion apparatus

Also Published As

Publication number Publication date
DE833741C (de) 1952-03-13
GB592505A (en) 1947-09-19
US2595999A (en) 1952-05-06
FR944726A (fr) 1949-04-13

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