CA983730A - Gas turbine combustor basket cooling - Google Patents

Gas turbine combustor basket cooling

Info

Publication number
CA983730A
CA983730A CA221,030A CA221030A CA983730A CA 983730 A CA983730 A CA 983730A CA 221030 A CA221030 A CA 221030A CA 983730 A CA983730 A CA 983730A
Authority
CA
Canada
Prior art keywords
gas turbine
turbine combustor
combustor basket
basket cooling
cooling
Prior art date
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
CA221,030A
Other versions
CA221030S (en
Inventor
Stephen R. Parker
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
Application granted granted Critical
Publication of CA983730A publication Critical patent/CA983730A/en
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
    • F23R3/045—Air inlet arrangements using pipes
CA221,030A 1974-03-27 1975-02-28 Gas turbine combustor basket cooling Expired CA983730A (en)

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
CA983730A true CA983730A (en) 1976-02-17

Family

ID=23807643

Family Applications (1)

Application Number Title Priority Date Filing Date
CA221,030A Expired CA983730A (en) 1974-03-27 1975-02-28 Gas turbine combustor basket cooling

Country Status (4)

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

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 (en) * 1976-02-06 1977-09-02 Snecma COMBUSTION CHAMBER BODY, ESPECIALLY FOR TURBOREACTORS
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 (en) * 1978-07-07 1983-06-13 日産自動車株式会社 Gas turbine combustor liner
JPS5932862U (en) * 1982-08-27 1984-02-29 三菱重工業株式会社 gas turbine combustor
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 (en) * 2001-11-15 2003-05-21 Siemens Aktiengesellschaft Gas turbine annular combustion chamber
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
US6722134B2 (en) 2002-09-18 2004-04-20 General Electric Company Linear surface concavity enhancement
US6761031B2 (en) 2002-09-18 2004-07-13 General Electric Company Double wall combustor liner segment with enhanced cooling
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
US6984102B2 (en) * 2003-11-19 2006-01-10 General Electric Company Hot gas path component with mesh and turbulated cooling
US7186084B2 (en) * 2003-11-19 2007-03-06 General Electric Company Hot gas path component with mesh and dimpled 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
DE102012015449A1 (en) 2012-08-03 2014-02-20 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine combustion chamber with mixed air openings and air guide elements in a modular design
DE102012015452A1 (en) * 2012-08-03 2014-04-24 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine combustion chamber wall for gas turbine engine, has mixed air openings formed by tubular air guide elements, which are fastened at wall and penetrate shingles arranged at inner side of wall
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
EP3044441B1 (en) * 2013-09-13 2022-07-27 Raytheon Technologies Corporation Shielding pockets for case holes
JP6456481B2 (en) 2014-08-26 2019-01-23 シーメンス エナジー インコーポレイテッド Film cooling hole array for an acoustic resonator in a gas turbine engine
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 (en) * 1966-07-08 1967-11-03 Snecma Improvements to turbo-reactors
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
JPS5235806B2 (en) 1977-09-12
JPS50133313A (en) 1975-10-22
IT1034535B (en) 1979-10-10
US3899882A (en) 1975-08-19

Similar Documents

Publication Publication Date Title
CA983730A (en) Gas turbine combustor basket cooling
CA1029664A (en) Air cooled turbine vanes
JPS5277913A (en) Gas turbine combustor
CA1012066A (en) Cooling system for a gas turbine
JPS521223A (en) Divided fan gas turbine engine
CA1010368A (en) Gas turbine rotor construction
JPS5257416A (en) Gas turbine with cooled rotor blade
JPS5364113A (en) Gas turbine
GB1544454A (en) Gas turbine engines
GB1551860A (en) Gas turbine engines
CA1018068A (en) Gas turbine bucket-root sidewall piece seals
GB1503457A (en) Gas turbine engines
JPS5243014A (en) Gas turbine combustor
GB1552990A (en) Gas turbine plant
GB1547203A (en) Cooled turbine or compressor buckets
JPS5236211A (en) Gas turbine engine
JPS5211314A (en) Gas turbine engine
JPS5274713A (en) Gas turbine engine combustor
JPS51120310A (en) Stator blade for gas turbine
JPS5331012A (en) Gas turbine blade
JPS5248713A (en) Gas turbine engine blade
CA1022462A (en) Gas turbine plant
JPS5214122A (en) Gas turbine engine
CA1013258A (en) Gas turbine stationary shroud seals
AU500628B1 (en) Gas shroud