JPS55155118A - Combustor for gas turbine - Google Patents

Combustor for gas turbine

Info

Publication number
JPS55155118A
JPS55155118A JP6546380A JP6546380A JPS55155118A JP S55155118 A JPS55155118 A JP S55155118A JP 6546380 A JP6546380 A JP 6546380A JP 6546380 A JP6546380 A JP 6546380A JP S55155118 A JPS55155118 A JP S55155118A
Authority
JP
Japan
Prior art keywords
combustor
gas turbine
turbine
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.)
Granted
Application number
JP6546380A
Other languages
English (en)
Other versions
JPS5914693B2 (ja
Inventor
Edowaado Peaasu Donarudo
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of JPS55155118A publication Critical patent/JPS55155118A/ja
Publication of JPS5914693B2 publication Critical patent/JPS5914693B2/ja
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
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
JP55065463A 1979-05-18 1980-05-19 ガスタ−ビンエンジン用燃焼装置 Expired JPS5914693B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB7917335 1979-05-18
GB7917335 1979-05-18

Publications (2)

Publication Number Publication Date
JPS55155118A true JPS55155118A (en) 1980-12-03
JPS5914693B2 JPS5914693B2 (ja) 1984-04-05

Family

ID=10505244

Family Applications (1)

Application Number Title Priority Date Filing Date
JP55065463A Expired JPS5914693B2 (ja) 1979-05-18 1980-05-19 ガスタ−ビンエンジン用燃焼装置

Country Status (4)

Country Link
US (1) US4365477A (ja)
EP (1) EP0019417B1 (ja)
JP (1) JPS5914693B2 (ja)
DE (1) DE3061595D1 (ja)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4928479A (en) * 1987-12-28 1990-05-29 Sundstrand Corporation Annular combustor with tangential cooling air injection
US5088287A (en) * 1989-07-13 1992-02-18 Sundstrand Corporation Combustor for a turbine
US5197289A (en) * 1990-11-26 1993-03-30 General Electric Company Double dome combustor
US5195315A (en) * 1991-01-14 1993-03-23 United Technologies Corporation Double dome combustor with counter rotating toroidal vortices and dual radial fuel injection
US5165226A (en) * 1991-08-09 1992-11-24 Pratt & Whitney Canada, Inc. Single vortex combustor arrangement
US5154060A (en) * 1991-08-12 1992-10-13 General Electric Company Stiffened double dome combustor
DE69306025T2 (de) * 1992-03-30 1997-05-28 Gen Electric Konstruktion eines Brennkammerdomes
US6089025A (en) * 1998-08-24 2000-07-18 General Electric Company Combustor baffle
US6286317B1 (en) * 1998-12-18 2001-09-11 General Electric Company Cooling nugget for a liner of a gas turbine engine combustor having trapped vortex cavity
US6711900B1 (en) * 2003-02-04 2004-03-30 Pratt & Whitney Canada Corp. Combustor liner V-band design
FR2866079B1 (fr) * 2004-02-05 2006-03-17 Snecma Moteurs Diffuseur pour turboreacteur
US7421843B2 (en) * 2005-01-15 2008-09-09 Siemens Power Generation, Inc. Catalytic combustor having fuel flow control responsive to measured combustion parameters
DE102006051286A1 (de) * 2006-10-26 2008-04-30 Deutsches Zentrum für Luft- und Raumfahrt e.V. Brennervorrichtung
US7794201B2 (en) * 2006-12-22 2010-09-14 General Electric Company Gas turbine engines including lean stator vanes and methods of assembling the same
US20100192578A1 (en) * 2009-01-30 2010-08-05 General Electric Company System and method for suppressing combustion instability in a turbomachine
FR2944584B1 (fr) * 2009-04-17 2014-08-22 Turbomeca Chambre de combustion avec deflecteur de refroidissement de fond de chambre brase.
US8381526B2 (en) * 2010-02-15 2013-02-26 General Electric Company Systems and methods of providing high pressure air to a head end of a combustor
WO2017165973A1 (en) 2016-03-30 2017-10-05 Marine Canada Acquisition Inc. Vehicle heater and controls therefor
RU201848U1 (ru) * 2020-08-12 2021-01-15 федеральное государственное бюджетное образовательное учреждение высшего образования "Ульяновский государственный технический университет" Камера сгорания газотурбинного двигателя с активной зоной охлаждения

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1039785B (de) * 1957-10-12 1958-09-25 Maschf Augsburg Nuernberg Ag Brennkammer mit hoher Waermebelastung, insbesondere fuer Verbrennung heizwertarmer, gasfoermiger Brennstoffe in Gasturbinenanlagen
US3808803A (en) * 1973-03-15 1974-05-07 Us Navy Anticarbon device for the scroll fuel carburetor
GB1429677A (en) * 1973-03-20 1976-03-24 Rolls Royce Gas turbine engine combustion equipment
US3937008A (en) * 1974-12-18 1976-02-10 United Technologies Corporation Low emission combustion chamber
FR2312654A1 (fr) * 1975-05-28 1976-12-24 Snecma Perfectionnements aux chambres de combustion pour moteurs a turbine a gaz
US4018043A (en) * 1975-09-19 1977-04-19 Avco Corporation Gas turbine engines with toroidal combustors
GB1600130A (en) * 1977-05-21 1981-10-14 Rolls Royce Combustion systems

Also Published As

Publication number Publication date
EP0019417B1 (en) 1983-01-12
DE3061595D1 (en) 1983-02-17
JPS5914693B2 (ja) 1984-04-05
US4365477A (en) 1982-12-28
EP0019417A1 (en) 1980-11-26

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