DE69632214D1 - Stirnwand für eine Gasturbinenbrennkammer - Google Patents

Stirnwand für eine Gasturbinenbrennkammer

Info

Publication number
DE69632214D1
DE69632214D1 DE69632214T DE69632214T DE69632214D1 DE 69632214 D1 DE69632214 D1 DE 69632214D1 DE 69632214 T DE69632214 T DE 69632214T DE 69632214 T DE69632214 T DE 69632214T DE 69632214 D1 DE69632214 D1 DE 69632214D1
Authority
DE
Germany
Prior art keywords
combustion chamber
gas turbine
front wall
turbine combustion
wall
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
DE69632214T
Other languages
English (en)
Other versions
DE69632214T2 (de
Inventor
Joseph D Monty
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 DE69632214D1 publication Critical patent/DE69632214D1/de
Application granted granted Critical
Publication of DE69632214T2 publication Critical patent/DE69632214T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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

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)
DE69632214T 1995-01-26 1996-01-11 Domeinrichtung für eine Gasturbinen-Brennkammer Expired - Lifetime DE69632214T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US378703 1995-01-26
US08/378,703 US5623827A (en) 1995-01-26 1995-01-26 Regenerative cooled dome assembly for a gas turbine engine combustor

Publications (2)

Publication Number Publication Date
DE69632214D1 true DE69632214D1 (de) 2004-05-27
DE69632214T2 DE69632214T2 (de) 2005-09-29

Family

ID=23494217

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69632214T Expired - Lifetime DE69632214T2 (de) 1995-01-26 1996-01-11 Domeinrichtung für eine Gasturbinen-Brennkammer

Country Status (3)

Country Link
US (1) US5623827A (de)
EP (1) EP0724119B1 (de)
DE (1) DE69632214T2 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107003003A (zh) * 2014-12-03 2017-08-01 赛峰飞机发动机公司 涡轮机燃烧室喷注系统的进气环和使包括所述进气环的喷注系统中的燃料雾化的方法

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FR3064050B1 (fr) 2017-03-14 2021-02-19 Safran Aircraft Engines Chambre de combustion d'une turbomachine
US10823416B2 (en) * 2017-08-10 2020-11-03 General Electric Company Purge cooling structure for combustor assembly
US10801726B2 (en) * 2017-09-21 2020-10-13 General Electric Company Combustor mixer purge cooling structure
US10941939B2 (en) * 2017-09-25 2021-03-09 General Electric Company Gas turbine assemblies and methods
US11221143B2 (en) * 2018-01-30 2022-01-11 General Electric Company Combustor and method of operation for improved emissions and durability
GB201802251D0 (en) * 2018-02-12 2018-03-28 Rolls Royce Plc An air swirler arrangement for a fuel injector of a combustion chamber
FR3078384B1 (fr) * 2018-02-28 2021-05-28 Safran Aircraft Engines Chambre de combustion a fond de chambre double
FR3081974B1 (fr) 2018-06-04 2020-06-19 Safran Aircraft Engines Chambre de combustion d'une turbomachine
FR3082284B1 (fr) * 2018-06-07 2020-12-11 Safran Aircraft Engines Chambre de combustion pour une turbomachine
US11187412B2 (en) * 2018-08-22 2021-11-30 General Electric Company Flow control wall assembly for heat engine
US11098730B2 (en) * 2019-04-12 2021-08-24 Rolls-Royce Corporation Deswirler assembly for a centrifugal compressor
CN113924444A (zh) * 2019-06-07 2022-01-11 赛峰直升机引擎公司 制造用于涡轮机的火焰管的方法
FR3097029B1 (fr) * 2019-06-07 2021-05-21 Safran Helicopter Engines Procédé de fabrication d’un tube à flamme pour une turbomachine
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107003003A (zh) * 2014-12-03 2017-08-01 赛峰飞机发动机公司 涡轮机燃烧室喷注系统的进气环和使包括所述进气环的喷注系统中的燃料雾化的方法

Also Published As

Publication number Publication date
EP0724119A3 (de) 1999-01-20
EP0724119A2 (de) 1996-07-31
EP0724119B1 (de) 2004-04-21
DE69632214T2 (de) 2005-09-29
US5623827A (en) 1997-04-29

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Legal Events

Date Code Title Description
8332 No legal effect for de
8370 Indication related to discontinuation of the patent is to be deleted