CH541716A - Gasturbinentriebwerk - Google Patents

Gasturbinentriebwerk

Info

Publication number
CH541716A
CH541716A CH1043171A CH1043171A CH541716A CH 541716 A CH541716 A CH 541716A CH 1043171 A CH1043171 A CH 1043171A CH 1043171 A CH1043171 A CH 1043171A CH 541716 A CH541716 A CH 541716A
Authority
CH
Switzerland
Prior art keywords
gas turbine
turbine engine
engine
gas
turbine
Prior art date
Application number
CH1043171A
Other languages
English (en)
Inventor
M Decorso Serafino
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 CH541716A publication Critical patent/CH541716A/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
    • F23R3/42—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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)
CH1043171A 1970-07-17 1971-07-15 Gasturbinentriebwerk CH541716A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US5582170A 1970-07-17 1970-07-17

Publications (1)

Publication Number Publication Date
CH541716A true CH541716A (de) 1973-09-15

Family

ID=22000363

Family Applications (1)

Application Number Title Priority Date Filing Date
CH1043171A CH541716A (de) 1970-07-17 1971-07-15 Gasturbinentriebwerk

Country Status (8)

Country Link
US (1) US3657883A (de)
JP (1) JPS5023450B1 (de)
CA (1) CA918937A (de)
CH (1) CH541716A (de)
DE (1) DE2133256A1 (de)
FR (1) FR2099438B1 (de)
GB (1) GB1303962A (de)
NL (1) NL7109893A (de)

Families Citing this family (37)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3742704A (en) * 1971-07-13 1973-07-03 Westinghouse Electric Corp Combustion chamber support structure
US4720970A (en) * 1982-11-05 1988-01-26 The United States Of America As Represented By The Secretary Of The Air Force Sector airflow variable geometry combustor
JPS61195214A (ja) * 1985-02-22 1986-08-29 Hitachi Ltd ガスタ−ビン燃焼器の空気流量調整機構
US5233822A (en) * 1991-01-31 1993-08-10 General Electric Company Method and system for the disassembly of an annular combustor
US5983641A (en) * 1997-04-30 1999-11-16 Mitsubishi Heavy Industries, Ltd. Tail pipe of gas turbine combustor and gas turbine combustor having the same tail pipe
US6691519B2 (en) * 2000-02-18 2004-02-17 Siemens Westinghouse Power Corporation Adaptable modular gas turbine power plant
US6672073B2 (en) 2002-05-22 2004-01-06 Siemens Westinghouse Power Corporation System and method for supporting fuel nozzles in a gas turbine combustor utilizing a support plate
US7200987B2 (en) * 2004-06-18 2007-04-10 General Electric Company Off-axis pulse detonation configuration for gas turbine engine
US7509807B2 (en) * 2004-08-13 2009-03-31 Siemens Energy, Inc. Concentric catalytic combustor
US8109098B2 (en) * 2006-05-04 2012-02-07 Siemens Energy, Inc. Combustor liner for gas turbine engine
EP2119966A1 (de) * 2008-05-15 2009-11-18 ALSTOM Technology Ltd Brennkammer mit reduzierten Kohlenstoffmonoxidemissionen
US7874138B2 (en) * 2008-09-11 2011-01-25 Siemens Energy, Inc. Segmented annular combustor
US8938976B2 (en) * 2011-05-20 2015-01-27 Siemens Energy, Inc. Structural frame for gas turbine combustion cap assembly
US20140083111A1 (en) * 2012-09-25 2014-03-27 United Technologies Corporation Gas turbine asymmetric fuel nozzle combustor
US9546601B2 (en) * 2012-11-20 2017-01-17 General Electric Company Clocked combustor can array
EP3015770B1 (de) * 2014-11-03 2020-07-01 Ansaldo Energia Switzerland AG Rohrbrennkammer
JP6625427B2 (ja) * 2015-12-25 2019-12-25 川崎重工業株式会社 ガスタービンエンジン
US10605459B2 (en) 2016-03-25 2020-03-31 General Electric Company Integrated combustor nozzle 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
US10641491B2 (en) 2016-03-25 2020-05-05 General Electric Company Cooling of integrated combustor nozzle of segmented annular combustion system
US10584876B2 (en) 2016-03-25 2020-03-10 General Electric Company Micro-channel cooling of integrated combustor nozzle of a 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
US11428413B2 (en) 2016-03-25 2022-08-30 General Electric Company Fuel injection module for segmented annular combustion system
US10563869B2 (en) 2016-03-25 2020-02-18 General Electric Company Operation and turndown of a segmented annular combustion system
US10724441B2 (en) 2016-03-25 2020-07-28 General Electric Company 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
US10690350B2 (en) 2016-11-28 2020-06-23 General Electric Company Combustor with axially staged fuel injection
US11156362B2 (en) 2016-11-28 2021-10-26 General Electric Company Combustor with axially staged fuel injection
US11015812B2 (en) * 2018-05-07 2021-05-25 Rolls-Royce North American Technologies Inc. Combustor bolted segmented architecture
RU2710642C1 (ru) * 2018-11-15 2019-12-30 Публичное Акционерное Общество "Одк-Сатурн" Трубчатая камера сгорания газотурбинного двигателя
US11371702B2 (en) 2020-08-31 2022-06-28 General Electric Company Impingement panel 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
US11460191B2 (en) 2020-08-31 2022-10-04 General Electric Company Cooling insert for a turbomachine
US11994292B2 (en) 2020-08-31 2024-05-28 General Electric Company Impingement cooling apparatus for turbomachine
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 (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE806613C (de) * 1947-02-24 1951-06-14 Cem Comp Electro Mec Anordnung der Verbrennungskammern von Gasturbinen
US2674090A (en) * 1950-03-21 1954-04-06 United Aircraft Corp Combustion chamber for gas turbines
DE1117348B (de) * 1954-02-27 1961-11-16 United Aircraft Corp Gasturbinentriebwerk
US3044263A (en) * 1959-05-21 1962-07-17 Dresser Ind Combustor with unitary liner
US3169367A (en) * 1963-07-18 1965-02-16 Westinghouse Electric Corp Combustion apparatus

Also Published As

Publication number Publication date
JPS5023450B1 (de) 1975-08-07
NL7109893A (de) 1972-01-19
CA918937A (en) 1973-01-16
DE2133256A1 (de) 1972-01-20
US3657883A (en) 1972-04-25
FR2099438A1 (de) 1972-03-17
GB1303962A (de) 1973-01-24
FR2099438B1 (de) 1975-07-11

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Legal Events

Date Code Title Description
PL Patent ceased