JPH0459531B2 - - Google Patents

Info

Publication number
JPH0459531B2
JPH0459531B2 JP61234696A JP23469686A JPH0459531B2 JP H0459531 B2 JPH0459531 B2 JP H0459531B2 JP 61234696 A JP61234696 A JP 61234696A JP 23469686 A JP23469686 A JP 23469686A JP H0459531 B2 JPH0459531 B2 JP H0459531B2
Authority
JP
Japan
Prior art keywords
sleeve
combustion chamber
ring flange
outer cylinder
flame tube
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 - Lifetime
Application number
JP61234696A
Other languages
English (en)
Japanese (ja)
Other versions
JPS6287733A (ja
Inventor
Minku Pauru
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.)
MTU Aero Engines AG
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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 MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Publication of JPS6287733A publication Critical patent/JPS6287733A/ja
Publication of JPH0459531B2 publication Critical patent/JPH0459531B2/ja
Granted 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
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Supercharger (AREA)
JP61234696A 1985-10-04 1986-10-03 ガスタ−ビン駆動装置用の燃焼室 Granted JPS6287733A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3535443A DE3535443C1 (de) 1985-10-04 1985-10-04 Brennkammer fuer ein Gasturbinentriebwerk,insbesondere Ringbrennkammer,mit mindestes einer Luftzufuhrbuchse
DE3535443.7 1985-10-04

Publications (2)

Publication Number Publication Date
JPS6287733A JPS6287733A (ja) 1987-04-22
JPH0459531B2 true JPH0459531B2 (enEXAMPLES) 1992-09-22

Family

ID=6282748

Family Applications (1)

Application Number Title Priority Date Filing Date
JP61234696A Granted JPS6287733A (ja) 1985-10-04 1986-10-03 ガスタ−ビン駆動装置用の燃焼室

Country Status (4)

Country Link
US (1) US4720979A (enEXAMPLES)
EP (1) EP0219722B1 (enEXAMPLES)
JP (1) JPS6287733A (enEXAMPLES)
DE (2) DE3535443C1 (enEXAMPLES)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2599821B1 (fr) * 1986-06-04 1988-09-02 Snecma Chambre de combustion pour turbomachines a orifices de melange assurant le positionnement de la paroi chaude sur la paroi froide
US4887432A (en) * 1988-10-07 1989-12-19 Westinghouse Electric Corp. Gas turbine combustion chamber with air scoops
US5144793A (en) * 1990-12-24 1992-09-08 United Technologies Corporation Integrated connector/airtube for a turbomachine's combustion chamber walls
JP3978541B2 (ja) * 2002-09-25 2007-09-19 現代自動車株式会社 エンジンのシリンダヘッドカバー及びその組立方法
US7000396B1 (en) * 2004-09-02 2006-02-21 General Electric Company Concentric fixed dilution and variable bypass air injection for a combustor
US9416682B2 (en) 2012-12-11 2016-08-16 United Technologies Corporation Turbine engine alignment assembly
US20150354819A1 (en) * 2013-01-16 2015-12-10 United Technologies Corporation Combustor Cooled Quench Zone Array
US11725817B2 (en) * 2021-06-30 2023-08-15 General Electric Company Combustor assembly with moveable interface dilution opening

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3007312A (en) * 1959-11-23 1961-11-07 Gen Motors Corp Combustion liner locater
FR1538394A (fr) * 1967-06-28 1968-09-06 Snecma Perfectionnements aux machines thermiques comprenant une chambre annulaire de combustion
GB1240009A (en) * 1968-07-27 1971-07-21 Leyland Gas Turbines Ltd Flame tube
US3545202A (en) * 1969-04-02 1970-12-08 United Aircraft Corp Wall structure and combustion holes for a gas turbine engine
US3874169A (en) * 1971-01-14 1975-04-01 Stal Laval Turbin Ab Combustion chamber for gas turbines
US3934408A (en) * 1974-04-01 1976-01-27 General Motors Corporation Ceramic combustion liner
GB2017827B (en) * 1978-04-04 1983-02-02 Gen Electric Combustor liner cooling
GB2089894B (en) * 1980-12-22 1985-08-14 Gen Electric Gas turbine engine air dispensing arrangement
US4454711A (en) * 1981-10-29 1984-06-19 Avco Corporation Self-aligning fuel nozzle assembly

Also Published As

Publication number Publication date
DE3661383D1 (en) 1989-01-12
EP0219722B1 (de) 1988-12-07
DE3535443C1 (de) 1986-11-20
US4720979A (en) 1988-01-26
EP0219722A1 (de) 1987-04-29
JPS6287733A (ja) 1987-04-22

Similar Documents

Publication Publication Date Title
JP4347657B2 (ja) ガスタービンと燃焼器
US5079915A (en) Heat protective lining for a passage in a turbojet engine
EP1391582B1 (en) Sealing structure for combustor liner
US6658853B2 (en) Seal structure for combustor liner
US6182451B1 (en) Gas turbine combustor waving ceramic combustor cans and an annular metallic combustor
EP2952813B1 (en) Combustor with tiled liner
JP3983603B2 (ja) セラミックマトリックス材料よりなる燃料室のための構造
US4169431A (en) Boiler
US7765809B2 (en) Combustor dome and methods of assembling such
US6647729B2 (en) Combustion chamber provided with a system for fixing the chamber end wall
US4543940A (en) Segmented radiant burner assembly and combustion process
JPH0459531B2 (enEXAMPLES)
US4850334A (en) Inner ceramic tube in particular for a glove finger-shaped radiant tube for recirculation
EP3760927B1 (en) Gas turbine engine combustor
US20030188537A1 (en) Advanced crossfire tube cooling scheme
US3672162A (en) Combustion chamber assembly for a gas turbine engine
US4623310A (en) Vaporized liquid fuel combustion apparatus
US4262487A (en) Double wall combustion chamber for a combustion turbine
EP0150791B1 (en) Sealing structure between at least one tube and a tube support plate
JPH0378535B2 (enEXAMPLES)
US5186006A (en) Mounting for ceramic scroll
JPH0771273A (ja) ガスタービン
CN100370177C (zh) 用于燃烧一种可燃烧的液态混合燃料的燃烧室
US10295272B2 (en) Rotary pre-heater for high temperature operation
JPH0814023A (ja) 排気ガス消音器