CA963674A - Gas turbine combustion liner - Google Patents

Gas turbine combustion liner

Info

Publication number
CA963674A
CA963674A CA157,902A CA157902A CA963674A CA 963674 A CA963674 A CA 963674A CA 157902 A CA157902 A CA 157902A CA 963674 A CA963674 A CA 963674A
Authority
CA
Canada
Prior art keywords
gas turbine
combustion liner
turbine combustion
liner
gas
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
CA157,902A
Other versions
CA157902S (en
Inventor
Albert J. Verdouw
John M. Vaught
Ralph B. Sweeney
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.)
Motors Liquidation Co
Original Assignee
Motors Liquidation Co
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 Motors Liquidation Co filed Critical Motors Liquidation Co
Application granted granted Critical
Publication of CA963674A publication Critical patent/CA963674A/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
    • F23R3/06—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)
CA157,902A 1972-02-25 1972-11-30 Gas turbine combustion liner Expired CA963674A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US22941172A 1972-02-25 1972-02-25

Publications (1)

Publication Number Publication Date
CA963674A true CA963674A (en) 1975-03-04

Family

ID=22861134

Family Applications (1)

Application Number Title Priority Date Filing Date
CA157,902A Expired CA963674A (en) 1972-02-25 1972-11-30 Gas turbine combustion liner

Country Status (3)

Country Link
US (1) US3751910A (en)
CA (1) CA963674A (en)
GB (1) GB1371003A (en)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3826082A (en) * 1973-03-30 1974-07-30 Gen Electric Combustion liner cooling slot stabilizing dimple
CH577627A5 (en) * 1974-04-03 1976-07-15 Bbc Sulzer Turbomaschinen
US4050241A (en) * 1975-12-22 1977-09-27 General Electric Company Stabilizing dimple for combustion liner cooling slot
US4527397A (en) * 1981-03-27 1985-07-09 Westinghouse Electric Corp. Turbine combustor having enhanced wall cooling for longer combustor life at high combustor outlet gas temperatures
US5259182A (en) * 1989-12-22 1993-11-09 Hitachi, Ltd. Combustion apparatus and combustion method therein
DE4232442A1 (en) * 1992-09-28 1994-03-31 Asea Brown Boveri Gas turbine combustion chamber
US5755093A (en) * 1995-05-01 1998-05-26 United Technologies Corporation Forced air cooled gas turbine exhaust liner
GB2441342B (en) * 2006-09-01 2009-03-18 Rolls Royce Plc Wall elements with apertures for gas turbine engine components
DE102007050664A1 (en) * 2007-10-24 2009-04-30 Man Turbo Ag Burner for a turbomachine, baffle for such a burner and a turbomachine with such a burner
US8511089B2 (en) * 2009-07-31 2013-08-20 Rolls-Royce Corporation Relief slot for combustion liner
EP3130854B1 (en) 2015-08-13 2020-06-24 Pratt & Whitney Canada Corp. Combustor shape cooling system
KR102071168B1 (en) * 2016-05-23 2020-01-29 미츠비시 히타치 파워 시스템즈 가부시키가이샤 Combustor, gas turbine
RU205407U1 (en) * 2020-12-08 2021-07-13 Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") Combustion tube with expansion slots

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3064425A (en) * 1959-10-05 1962-11-20 Gen Motors Corp Combustion liner
US3307354A (en) * 1965-10-01 1967-03-07 Gen Electric Cooling structure for overlapped panels
US3420058A (en) * 1967-01-03 1969-01-07 Gen Electric Combustor liners
US3408812A (en) * 1967-02-24 1968-11-05 Gen Electric Cooled joint construction for combustion wall means
US3485043A (en) * 1968-02-01 1969-12-23 Gen Electric Shingled combustion liner
US3589128A (en) * 1970-02-02 1971-06-29 Avco Corp Cooling arrangement for a reverse flow gas turbine combustor

Also Published As

Publication number Publication date
GB1371003A (en) 1974-10-23
US3751910A (en) 1973-08-14

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