FR2121779B1 - - Google Patents

Info

Publication number
FR2121779B1
FR2121779B1 FR7200919A FR7200919A FR2121779B1 FR 2121779 B1 FR2121779 B1 FR 2121779B1 FR 7200919 A FR7200919 A FR 7200919A FR 7200919 A FR7200919 A FR 7200919A FR 2121779 B1 FR2121779 B1 FR 2121779B1
Authority
FR
France
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
FR7200919A
Other languages
French (fr)
Other versions
FR2121779A1 (de
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.)
CBS Corp
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 FR2121779A1 publication Critical patent/FR2121779A1/fr
Application granted granted Critical
Publication of FR2121779B1 publication Critical patent/FR2121779B1/fr
Expired legal-status Critical Current

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
    • F23R3/02—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

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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR7200919A 1971-01-13 1972-01-12 Expired FR2121779B1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10604171A 1971-01-13 1971-01-13

Publications (2)

Publication Number Publication Date
FR2121779A1 FR2121779A1 (de) 1972-08-25
FR2121779B1 true FR2121779B1 (de) 1974-11-08

Family

ID=22309157

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7200919A Expired FR2121779B1 (de) 1971-01-13 1972-01-12

Country Status (8)

Country Link
US (1) US3702058A (de)
CA (1) CA942513A (de)
CH (1) CH547996A (de)
DE (1) DE2161644A1 (de)
FR (1) FR2121779B1 (de)
GB (1) GB1312907A (de)
IT (1) IT946524B (de)
NL (1) NL7118118A (de)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4174608A (en) * 1972-08-15 1979-11-20 Stal-Laval Turbin Ab Combustion chamber for a gas turbine
FR2340453A1 (fr) * 1976-02-06 1977-09-02 Snecma Corps de chambre de combustion, notamment pour turboreacteurs
US4132066A (en) * 1977-09-23 1979-01-02 United Technologies Corporation Combustor liner for gas turbine engine
US4262487A (en) * 1979-02-01 1981-04-21 Westinghouse Electric Corp. Double wall combustion chamber for a combustion turbine
US4292810A (en) * 1979-02-01 1981-10-06 Westinghouse Electric Corp. Gas turbine combustion chamber
US4413477A (en) * 1980-12-29 1983-11-08 General Electric Company Liner assembly for gas turbine combustor
US4845940A (en) * 1981-02-27 1989-07-11 Westinghouse Electric Corp. Low NOx rich-lean combustor especially useful in gas turbines
US4413470A (en) * 1981-03-05 1983-11-08 Electric Power Research Institute, Inc. Catalytic combustion system for a stationary combustion turbine having a transition duct mounted catalytic element
US4407205A (en) * 1982-04-30 1983-10-04 Beaufrere Albert H Regeneratively cooled coal combustor/gasifier with integral dry ash removal
US4642993A (en) * 1985-04-29 1987-02-17 Avco Corporation Combustor liner wall
US4887432A (en) * 1988-10-07 1989-12-19 Westinghouse Electric Corp. Gas turbine combustion chamber with air scoops
JPH04123865A (ja) * 1990-09-13 1992-04-23 Hitachi Ltd 燃焼器ライナーの製造方法、溶着方法、および溶着装置
DE4244303A1 (de) * 1992-12-28 1994-06-30 Abb Research Ltd Vorrichtung zur Prallkühlung
JP3415663B2 (ja) * 1992-12-28 2003-06-09 アルストム 冷却面を衝撃式に冷却するための装置
US5327727A (en) * 1993-04-05 1994-07-12 General Electric Company Micro-grooved heat transfer combustor wall
US6018950A (en) * 1997-06-13 2000-02-01 Siemens Westinghouse Power Corporation Combustion turbine modular cooling panel
EP1284391A1 (de) * 2001-08-14 2003-02-19 Siemens Aktiengesellschaft Brennkammeranordnung für Gasturbinen
EP1312865A1 (de) * 2001-11-15 2003-05-21 Siemens Aktiengesellschaft Ringbrennkammer für eine Gasturbine
US7377116B2 (en) * 2005-04-28 2008-05-27 Siemens Power Generation, Inc. Gas turbine combustor barrier structures for spring clips
US7594401B1 (en) * 2008-04-10 2009-09-29 General Electric Company Combustor seal having multiple cooling fluid pathways
US8549861B2 (en) * 2009-01-07 2013-10-08 General Electric Company Method and apparatus to enhance transition duct cooling in a gas turbine engine
US8667801B2 (en) 2010-09-08 2014-03-11 Siemens Energy, Inc. Combustor liner assembly with enhanced cooling system
ES2427440T3 (es) * 2011-03-15 2013-10-30 Siemens Aktiengesellschaft Cámara de combustión de turbina de gas
US9366438B2 (en) * 2013-02-14 2016-06-14 Siemens Aktiengesellschaft Flow sleeve inlet assembly in a gas turbine engine
US20220018541A1 (en) * 2020-07-16 2022-01-20 Raytheon Technologies Corporation Article and method for manufacturing an expanded combustor liner

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH229934A (de) * 1942-10-06 1943-11-30 Bbc Brown Boveri & Cie Gasturbinenanlage.
FR945486A (fr) * 1946-04-03 1949-05-05 Westinghouse Electric Corp Perfectionnements aux appareils de combustion pour turbines à gaz
US2610467A (en) * 1946-04-03 1952-09-16 Westinghouse Electric Corp Combustion chamber having telescoping walls and corrugated spacers
GB759489A (en) * 1953-02-26 1956-10-17 Rolls Royce Improvements in or relating to gas-turbine engine combustion equipment
US3169367A (en) * 1963-07-18 1965-02-16 Westinghouse Electric Corp Combustion apparatus
GB998755A (en) * 1964-05-07 1965-07-21 Rolls Royce Improvements in or relating to combustion equipment
US3545202A (en) * 1969-04-02 1970-12-08 United Aircraft Corp Wall structure and combustion holes for a gas turbine engine
US3572031A (en) * 1969-07-11 1971-03-23 United Aircraft Corp Variable area cooling passages for gas turbine burners

Also Published As

Publication number Publication date
CA942513A (en) 1974-02-26
NL7118118A (de) 1972-07-17
IT946524B (it) 1973-05-21
FR2121779A1 (de) 1972-08-25
US3702058A (en) 1972-11-07
GB1312907A (en) 1973-04-11
CH547996A (de) 1974-04-11
DE2161644A1 (de) 1972-07-20

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Legal Events

Date Code Title Description
ST Notification of lapse