CH547996A - COMBUSTION CHAMBER FOR GAS TURBINES. - Google Patents

COMBUSTION CHAMBER FOR GAS TURBINES.

Info

Publication number
CH547996A
CH547996A CH1858971A CH1858971A CH547996A CH 547996 A CH547996 A CH 547996A CH 1858971 A CH1858971 A CH 1858971A CH 1858971 A CH1858971 A CH 1858971A CH 547996 A CH547996 A CH 547996A
Authority
CH
Switzerland
Prior art keywords
combustion chamber
gas turbines
turbines
gas
combustion
Prior art date
Application number
CH1858971A
Other languages
German (de)
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 CH547996A publication Critical patent/CH547996A/en

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
    • F23R3/08Arrangement 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)
CH1858971A 1971-01-13 1971-12-20 COMBUSTION CHAMBER FOR GAS TURBINES. CH547996A (en)

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
CH547996A true CH547996A (en) 1974-04-11

Family

ID=22309157

Family Applications (1)

Application Number Title Priority Date Filing Date
CH1858971A CH547996A (en) 1971-01-13 1971-12-20 COMBUSTION CHAMBER FOR GAS TURBINES.

Country Status (8)

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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4244303A1 (en) * 1992-12-28 1994-06-30 Abb Research Ltd Impact cooling system for cooling surface e.g. of combustion chamber wall
US5467815A (en) * 1992-12-28 1995-11-21 Abb Research Ltd. Apparatus for impingement cooling

Families Citing this family (23)

* 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 (en) * 1976-02-06 1977-09-02 Snecma COMBUSTION CHAMBER BODY, ESPECIALLY FOR TURBOREACTORS
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 (en) * 1990-09-13 1992-04-23 Hitachi Ltd Manufacture of combustor liner, depositing method and depositing device
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 (en) * 2001-08-14 2003-02-19 Siemens Aktiengesellschaft Combustion chamber for gas turbines
EP1312865A1 (en) * 2001-11-15 2003-05-21 Siemens Aktiengesellschaft Gas turbine annular combustion chamber
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 (en) * 2011-03-15 2013-10-30 Siemens Aktiengesellschaft Gas turbine combustion chamber
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 (en) * 1942-10-06 1943-11-30 Bbc Brown Boveri & Cie Gas turbine plant.
FR945486A (en) * 1946-04-03 1949-05-05 Westinghouse Electric Corp Improvements to combustion devices for gas turbines
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

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4244303A1 (en) * 1992-12-28 1994-06-30 Abb Research Ltd Impact cooling system for cooling surface e.g. of combustion chamber wall
US5467815A (en) * 1992-12-28 1995-11-21 Abb Research Ltd. Apparatus for impingement cooling

Also Published As

Publication number Publication date
FR2121779B1 (en) 1974-11-08
NL7118118A (en) 1972-07-17
GB1312907A (en) 1973-04-11
US3702058A (en) 1972-11-07
CA942513A (en) 1974-02-26
FR2121779A1 (en) 1972-08-25
IT946524B (en) 1973-05-21
DE2161644A1 (en) 1972-07-20

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Legal Events

Date Code Title Description
PL Patent ceased