DE2414376A1 - Kuehlschlitzanordnung fuer einen brennkammereinsatz - Google Patents

Kuehlschlitzanordnung fuer einen brennkammereinsatz

Info

Publication number
DE2414376A1
DE2414376A1 DE2414376A DE2414376A DE2414376A1 DE 2414376 A1 DE2414376 A1 DE 2414376A1 DE 2414376 A DE2414376 A DE 2414376A DE 2414376 A DE2414376 A DE 2414376A DE 2414376 A1 DE2414376 A1 DE 2414376A1
Authority
DE
Germany
Prior art keywords
lip
depth
insert
arrangement according
combustion chamber
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.)
Pending
Application number
DE2414376A
Other languages
German (de)
English (en)
Inventor
Robert John Smuland
Richard Kenneth Ward
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.)
General Electric Co
Original Assignee
General Electric 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 General Electric Co filed Critical General Electric Co
Publication of DE2414376A1 publication Critical patent/DE2414376A1/de
Pending legal-status Critical Current

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
    • F23R3/06Arrangement of apertures along the flame tube
    • F23R3/08Arrangement 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)
  • Spray-Type Burners (AREA)
DE2414376A 1973-03-30 1974-03-26 Kuehlschlitzanordnung fuer einen brennkammereinsatz Pending DE2414376A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00346595A US3826082A (en) 1973-03-30 1973-03-30 Combustion liner cooling slot stabilizing dimple

Publications (1)

Publication Number Publication Date
DE2414376A1 true DE2414376A1 (de) 1974-10-17

Family

ID=23360142

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2414376A Pending DE2414376A1 (de) 1973-03-30 1974-03-26 Kuehlschlitzanordnung fuer einen brennkammereinsatz

Country Status (7)

Country Link
US (1) US3826082A (enrdf_load_stackoverflow)
JP (1) JPS5025918A (enrdf_load_stackoverflow)
BE (1) BE813091A (enrdf_load_stackoverflow)
CA (1) CA996761A (enrdf_load_stackoverflow)
DE (1) DE2414376A1 (enrdf_load_stackoverflow)
FR (1) FR2223554A1 (enrdf_load_stackoverflow)
IT (1) IT1003927B (enrdf_load_stackoverflow)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0151918A3 (en) * 1984-02-15 1987-03-11 National Aeronautics And Space Administration Method and apparatus for cooling high temperature structures with a fluid coolant

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4109459A (en) * 1974-07-19 1978-08-29 General Electric Company Double walled impingement cooled combustor
US4050241A (en) * 1975-12-22 1977-09-27 General Electric Company Stabilizing dimple for combustion liner cooling slot
CH620372A5 (en) * 1976-02-05 1980-11-28 Metaux Speciaux Sa Process for the treatment of spent catalysts with a view to the recovery of molybdenum
JPS6115418Y2 (enrdf_load_stackoverflow) * 1977-09-12 1986-05-13
FR2510541A2 (fr) * 1977-09-30 1983-02-04 Pechiney Ugine Kuhlmann Uran Procede de valorisation du molybdene a partir de solutions molybdeniferes contenant des carbonate, sulfate, hydroxyde ou hydrogenocarbonate alcalins, ainsi que, eventuellement, de l'uranium
US4259842A (en) * 1978-12-11 1981-04-07 General Electric Company Combustor liner slot with cooled props
FR2450349A1 (fr) * 1979-03-01 1980-09-26 Snecma Perfectionnement au refroidissement des parois de chambres de combustion par pellicule d'air
US4380906A (en) * 1981-01-22 1983-04-26 United Technologies Corporation Combustion liner cooling scheme
US4688310A (en) * 1983-12-19 1987-08-25 General Electric Company Fabricated liner article and method
US4833881A (en) * 1984-12-17 1989-05-30 General Electric Company Gas turbine engine augmentor
JPH0637976B2 (ja) * 1985-04-05 1994-05-18 工業技術院長 ガスタービン用燃焼器の尾筒の製造方法
DE3540942A1 (de) * 1985-11-19 1987-05-21 Mtu Muenchen Gmbh Umkehrbrennkammer, insbesondere umkehrringbrennkammer, fuer gasturbinentriebwerke, mit mindestens einer flammrohrwandfilmkuehleinrichtung
US5331803A (en) * 1989-07-24 1994-07-26 Sundstrand Corporation Method of obtaining a desired temperature profile in a turbine engine and turbine engine incorporating the same
JP2928607B2 (ja) * 1989-12-22 1999-08-03 株式会社日立製作所 燃焼装置及びその燃焼方法
US5259182A (en) * 1989-12-22 1993-11-09 Hitachi, Ltd. Combustion apparatus and combustion method therein
GB2261281B (en) * 1991-11-08 1995-01-18 Bmw Rolls Royce Gmbh A combustion-chamber casting for a gas turbine
RU2319075C9 (ru) * 2006-05-10 2008-05-27 Открытое акционерное общество "Климов" Жаровая труба камеры сгорания
US20100107645A1 (en) * 2008-10-31 2010-05-06 General Electric Company Combustor liner cooling flow disseminator and related method
KR101556532B1 (ko) * 2014-01-16 2015-10-01 두산중공업 주식회사 냉각슬리브를 포함하는 라이너, 플로우슬리브 및 가스터빈연소기
US10012389B2 (en) * 2014-05-08 2018-07-03 United Technologies Corporation Case with integral heat shielding
DE102016201452A1 (de) * 2016-02-01 2017-08-03 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinenbrennkammer mit Wandkonturierung
JP6639063B2 (ja) * 2016-05-23 2020-02-05 三菱日立パワーシステムズ株式会社 燃焼器、ガスタービン
JP7393262B2 (ja) * 2020-03-23 2023-12-06 三菱重工業株式会社 燃焼器、及びこれを備えるガスタービン
RU205407U1 (ru) * 2020-12-08 2021-07-13 Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") Жаровая труба с компенсационными щелями
CN117469698A (zh) 2022-07-21 2024-01-30 通用电气公司 燃烧衬里的性能因数

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3307354A (en) * 1965-10-01 1967-03-07 Gen Electric Cooling structure for overlapped panels
US3589127A (en) * 1969-02-04 1971-06-29 Gen Electric Combustion apparatus
US3745766A (en) * 1971-10-26 1973-07-17 Avco Corp Variable geometry for controlling the flow of air to a combustor
US3751910A (en) * 1972-02-25 1973-08-14 Gen Motors Corp Combustion liner

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0151918A3 (en) * 1984-02-15 1987-03-11 National Aeronautics And Space Administration Method and apparatus for cooling high temperature structures with a fluid coolant

Also Published As

Publication number Publication date
CA996761A (en) 1976-09-14
US3826082A (en) 1974-07-30
BE813091A (fr) 1974-07-15
FR2223554A1 (enrdf_load_stackoverflow) 1974-10-25
IT1003927B (it) 1976-06-10
JPS5025918A (enrdf_load_stackoverflow) 1975-03-18

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