FR2713749B1 - Chambre de post combustion de turbine à gaz. - Google Patents

Chambre de post combustion de turbine à gaz.

Info

Publication number
FR2713749B1
FR2713749B1 FR9315054A FR9315054A FR2713749B1 FR 2713749 B1 FR2713749 B1 FR 2713749B1 FR 9315054 A FR9315054 A FR 9315054A FR 9315054 A FR9315054 A FR 9315054A FR 2713749 B1 FR2713749 B1 FR 2713749B1
Authority
FR
France
Prior art keywords
post
combustion chamber
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.)
Expired - Fee Related
Application number
FR9315054A
Other languages
English (en)
Other versions
FR2713749A1 (fr
Inventor
Capelle Jean-Yves
Desaulty Michel
Le Letty Eric
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR9315054A priority Critical patent/FR2713749B1/fr
Publication of FR2713749A1 publication Critical patent/FR2713749A1/fr
Application granted granted Critical
Publication of FR2713749B1 publication Critical patent/FR2713749B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow
    • F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/78—Other construction of jet pipes
    • F02K1/82—Jet pipe walls, e.g. liners
    • F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infra-red radiation suppressors
    • 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
FR9315054A 1993-12-15 1993-12-15 Chambre de post combustion de turbine à gaz. Expired - Fee Related FR2713749B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR9315054A FR2713749B1 (fr) 1993-12-15 1993-12-15 Chambre de post combustion de turbine à gaz.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR9315054A FR2713749B1 (fr) 1993-12-15 1993-12-15 Chambre de post combustion de turbine à gaz.

Publications (2)

Publication Number Publication Date
FR2713749A1 FR2713749A1 (fr) 1995-06-16
FR2713749B1 true FR2713749B1 (fr) 1996-01-12

Family

ID=9453944

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9315054A Expired - Fee Related FR2713749B1 (fr) 1993-12-15 1993-12-15 Chambre de post combustion de turbine à gaz.

Country Status (1)

Country Link
FR (1) FR2713749B1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105403243A (zh) * 2015-08-25 2016-03-16 中国人民解放军国防科学技术大学 燃烧室水冷壁面上测温测压装置及其加工方法

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7798765B2 (en) * 2007-04-12 2010-09-21 United Technologies Corporation Out-flow margin protection for a gas turbine engine

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB712633A (en) * 1952-07-22 1954-07-28 Rolls Royce Improvements relating to gas-turbine engines
US2941356A (en) * 1957-03-01 1960-06-21 United Aircraft Corp Variable pressure wave absorption for combustion chambers
DE3606286A1 (de) * 1985-03-04 1986-09-04 General Electric Co., Schenectady, N.Y. Verfahren und einrichtung zum steuern des kuehlmittelstroemungsflusses in einer nachbrennerauskleidung
US4926633A (en) * 1989-06-27 1990-05-22 The United States Of America As Represented By The Secretary Of The Air Force Coolant pressure regulating apparatus

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105403243A (zh) * 2015-08-25 2016-03-16 中国人民解放军国防科学技术大学 燃烧室水冷壁面上测温测压装置及其加工方法
CN105403243B (zh) * 2015-08-25 2020-08-11 中国人民解放军国防科技大学 燃烧室水冷壁面上测温测压装置及其加工方法

Also Published As

Publication number Publication date
FR2713749A1 (fr) 1995-06-16

Similar Documents

Publication Publication Date Title
DE69312208T2 (de) Gasturbinenbrennkammer
DE59610298D1 (de) Gasturbinenringbrennkammer
FR2708338B1 (fr) Brûleur de turbine à gaz.
DE59306732D1 (de) Gasturbinenbrennkammer
DE69205576D1 (de) Gasturbinenbrennkammer.
DE69101682D1 (de) Gasturbinenbrennkammer.
DE69102032D1 (de) Gasturbinenbrennkammer.
DE69111614D1 (de) Gasturbinenbrennkammer und deren arbeitsweise.
DE68901320D1 (de) Gasturbinenbrennkammer.
FR2699963B1 (fr) Générateur de gaz à combustion rapprochée.
DE69301890T2 (de) Gasturbinenbrennkammer
FR2697287B1 (fr) Diffuseur d'échappement de turbine à gaz.
DE69204280T2 (de) Gasturbinenbrennkammer.
DE69404566D1 (de) Brennkammer mit Gasabscheider
DE68903138D1 (de) Gasturbinenbrennkammer.
DE69115879T2 (de) Gasturbinen-brennkammersystem
DE69223126T2 (de) Gasturbinenbrennkammer
DE69502984D1 (de) Gasturbinenbrennkammer
DE59604179D1 (de) Katalytische gasturbinenbrennkammer
FR2713749B1 (fr) Chambre de post combustion de turbine à gaz.
DE59307265D1 (de) Gasturbinenbrennkammer
FR2708716B1 (fr) Agencement en étoile de brûleurs à gaz.
KR950009414U (ko) 가스보일러의 연소실 구조
KR950009487U (ko) 연소실이 분리된 가스보일러
KR970044480U (ko) 가스보일러의 연소실 구조

Legal Events

Date Code Title Description
CD Change of name or company name
TP Transmission of property
ST Notification of lapse