IT1034535B - Raffreddamento del tubo di fiamma di una turbina a gas - Google Patents

Raffreddamento del tubo di fiamma di una turbina a gas

Info

Publication number
IT1034535B
IT1034535B IT21651/75A IT2165175A IT1034535B IT 1034535 B IT1034535 B IT 1034535B IT 21651/75 A IT21651/75 A IT 21651/75A IT 2165175 A IT2165175 A IT 2165175A IT 1034535 B IT1034535 B IT 1034535B
Authority
IT
Italy
Prior art keywords
cooling
gas turbine
flame tube
flame
tube
Prior art date
Application number
IT21651/75A
Other languages
English (en)
Italian (it)
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
Application granted granted Critical
Publication of IT1034535B publication Critical patent/IT1034535B/it

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
    • F23R3/045Air inlet arrangements using pipes

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
IT21651/75A 1974-03-27 1975-03-26 Raffreddamento del tubo di fiamma di una turbina a gas IT1034535B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US455161A US3899882A (en) 1974-03-27 1974-03-27 Gas turbine combustor basket cooling

Publications (1)

Publication Number Publication Date
IT1034535B true IT1034535B (it) 1979-10-10

Family

ID=23807643

Family Applications (1)

Application Number Title Priority Date Filing Date
IT21651/75A IT1034535B (it) 1974-03-27 1975-03-26 Raffreddamento del tubo di fiamma di una turbina a gas

Country Status (4)

Country Link
US (1) US3899882A (ko)
JP (1) JPS5235806B2 (ko)
CA (1) CA983730A (ko)
IT (1) IT1034535B (ko)

Families Citing this family (45)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1490145A (en) * 1974-09-11 1977-10-26 Mtu Muenchen Gmbh Gas turbine engine
FR2340453A1 (fr) * 1976-02-06 1977-09-02 Snecma Corps de chambre de combustion, notamment pour turboreacteurs
JPS53104019A (en) * 1977-02-23 1978-09-09 Hitachi Ltd Gas turbine combustor
US4192138A (en) * 1977-08-29 1980-03-11 Westinghouse Electric Corp. Gas turbine combustor air inlet
US4132066A (en) * 1977-09-23 1979-01-02 United Technologies Corporation Combustor liner for gas turbine engine
GB2017827B (en) * 1978-04-04 1983-02-02 Gen Electric Combustor liner cooling
JPS5827264Y2 (ja) * 1978-07-07 1983-06-13 日産自動車株式会社 ガスタ−ビンの燃焼器ライナ
JPS5932862U (ja) * 1982-08-27 1984-02-29 三菱重工業株式会社 ガスタ−ビン燃焼器
GB8703101D0 (en) * 1987-02-11 1987-03-18 Secr Defence Gas turbine engine combustion chambers
US4875339A (en) * 1987-11-27 1989-10-24 General Electric Company Combustion chamber liner insert
US4887432A (en) * 1988-10-07 1989-12-19 Westinghouse Electric Corp. Gas turbine combustion chamber with air scoops
US6101814A (en) * 1999-04-15 2000-08-15 United Technologies Corporation Low emissions can combustor with dilution hole arrangement for a turbine engine
US6494044B1 (en) 1999-11-19 2002-12-17 General Electric Company Aerodynamic devices for enhancing sidepanel cooling on an impingement cooled transition duct and related method
GB2379499B (en) * 2001-09-11 2004-01-28 Rolls Royce Plc Gas turbine engine combustor
EP1312865A1 (de) * 2001-11-15 2003-05-21 Siemens Aktiengesellschaft Ringbrennkammer für eine Gasturbine
US6681577B2 (en) * 2002-01-16 2004-01-27 General Electric Company Method and apparatus for relieving stress in a combustion case in a gas turbine engine
US6761031B2 (en) 2002-09-18 2004-07-13 General Electric Company Double wall combustor liner segment with enhanced cooling
US6722134B2 (en) 2002-09-18 2004-04-20 General Electric Company Linear surface concavity enhancement
US7104067B2 (en) * 2002-10-24 2006-09-12 General Electric Company Combustor liner with inverted turbulators
US6681578B1 (en) * 2002-11-22 2004-01-27 General Electric Company Combustor liner with ring turbulators and related method
GB2399408B (en) * 2003-03-14 2006-02-22 Rolls Royce Plc Gas turbine engine combustor
US7186084B2 (en) * 2003-11-19 2007-03-06 General Electric Company Hot gas path component with mesh and dimpled cooling
US6984102B2 (en) * 2003-11-19 2006-01-10 General Electric Company Hot gas path component with mesh and turbulated cooling
GB0601413D0 (en) * 2006-01-25 2006-03-08 Rolls Royce Plc Wall elements for gas turbine engine combustors
US8281600B2 (en) * 2007-01-09 2012-10-09 General Electric Company Thimble, sleeve, and method for cooling a combustor assembly
US8151570B2 (en) * 2007-12-06 2012-04-10 Alstom Technology Ltd Transition duct cooling feed tubes
US8627669B2 (en) 2008-07-18 2014-01-14 Siemens Energy, Inc. Elimination of plate fins in combustion baskets by CMC insulation installed by shrink fit
US20100050649A1 (en) * 2008-09-04 2010-03-04 Allen David B Combustor device and transition duct assembly
US8490400B2 (en) * 2008-09-15 2013-07-23 Siemens Energy, Inc. Combustor assembly comprising a combustor device, a transition duct and a flow conditioner
US8161752B2 (en) * 2008-11-20 2012-04-24 Honeywell International Inc. Combustors with inserts between dual wall liners
US20100223930A1 (en) * 2009-03-06 2010-09-09 General Electric Company Injection device for a turbomachine
US20100269513A1 (en) * 2009-04-23 2010-10-28 General Electric Company Thimble Fan for a Combustion System
US8397511B2 (en) * 2009-05-19 2013-03-19 General Electric Company System and method for cooling a wall of a gas turbine combustor
US20120036859A1 (en) * 2010-08-12 2012-02-16 General Electric Company Combustor transition piece with dilution sleeves and related method
US8650852B2 (en) * 2011-07-05 2014-02-18 General Electric Company Support assembly for transition duct in turbine system
DE102012015452A1 (de) * 2012-08-03 2014-04-24 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenbrennkammerwand mit Mischluftöffnungen und Luftleitelementen
DE102012015449A1 (de) * 2012-08-03 2014-02-20 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenbrennkammer mit Mischluftöffnungen und Luftleitelementen in modularer Bauweise
US9255835B2 (en) 2012-08-22 2016-02-09 Siemens Energy, Inc. System for remote vibration detection on combustor basket and transition in gas turbines
US9255526B2 (en) 2012-08-23 2016-02-09 Siemens Energy, Inc. System and method for on line monitoring within a gas turbine combustor section
US10690006B2 (en) * 2013-09-13 2020-06-23 Raytheon Technologies Corporation Shielding pockets for case holes
WO2016032434A1 (en) 2014-08-26 2016-03-03 Siemens Energy, Inc. Film cooling hole arrangement for acoustic resonators in gas turbine engines
EP2993404B1 (en) * 2014-09-08 2019-03-13 Ansaldo Energia Switzerland AG Dilution gas or air mixer for a combustor of a gas turbine
US11255543B2 (en) * 2018-08-07 2022-02-22 General Electric Company Dilution structure for gas turbine engine combustor
US11085639B2 (en) * 2018-12-27 2021-08-10 Rolls-Royce North American Technologies Inc. Gas turbine combustor liner with integral chute made by additive manufacturing process
GB201902693D0 (en) * 2019-02-28 2019-04-17 Rolls Royce Plc Combustion liner and gas turbine engine comprising a combustion liner

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3121996A (en) * 1961-10-02 1964-02-25 Lucas Industries Ltd Liquid fuel combustion apparatus
FR1500110A (fr) * 1966-07-08 1967-11-03 Snecma Perfectionnements aux turbo-réacteurs
GB1271084A (en) * 1968-05-13 1972-04-19 T C Borrie Ltd Improvements in or relating to cartridge-operated hand tools

Also Published As

Publication number Publication date
JPS50133313A (ko) 1975-10-22
CA983730A (en) 1976-02-17
JPS5235806B2 (ko) 1977-09-12
US3899882A (en) 1975-08-19

Similar Documents

Publication Publication Date Title
IT1034535B (it) Raffreddamento del tubo di fiamma di una turbina a gas
BE802514A (fr) Compositions engendrant un gaz
IT1067171B (it) Motore a turbina a gas con supporto perfezionato del condotto di transizione
IT941241B (it) Manicotto refrigerante di raccordo di un bruciatore di turbina a gas
DK331675A (da) Gasfyrtoj af engangstypen
IT975453B (it) Tubo di fiamma per la camera di com bustione di una turbina a gas
BR7506353A (pt) Conexao aperfeicoada de tubo
CH520267A (fr) Turbine à gaz
IT961918B (it) Tubo a fiamma per motori a turbina a gas
BE824390A (nl) Gasbrander
SE7513380L (sv) Hogtrycksgasurladdningslampa
BE873775Q (fr) Bruleur a gaz
BE826108A (fr) Turbine a gaz
FR2291628A1 (fr) Laser a gaz
BE782487A (fr) Laser a gaz
IT1044414B (it) Perfezionamento negle accendini a gas
IT1004606B (it) Bruciatore a gas
IT944799B (it) Tubo di fiamma per turbine a gas
IT1031255B (it) Tubo di prelevamento
BE768016A (fr) Bruleur a gaz
CH509681A (fr) Tube laser à gaz
IT962685B (it) Dispositivo di illuminazione con tubo a scarica di gas con funzio namento ad impulsi
BE823193A (fr) Laser a gaz
BE826041A (fr) Turbine a gaz
SE7513826L (sv) Gasbrennarverktyg