FR2465080B1 - - Google Patents

Info

Publication number
FR2465080B1
FR2465080B1 FR7923489A FR7923489A FR2465080B1 FR 2465080 B1 FR2465080 B1 FR 2465080B1 FR 7923489 A FR7923489 A FR 7923489A FR 7923489 A FR7923489 A FR 7923489A FR 2465080 B1 FR2465080 B1 FR 2465080B1
Authority
FR
France
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
Application number
FR7923489A
Other languages
French (fr)
Other versions
FR2465080A1 (fr
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 FR7923489A priority Critical patent/FR2465080A1/fr
Publication of FR2465080A1 publication Critical patent/FR2465080A1/fr
Application granted granted Critical
Publication of FR2465080B1 publication Critical patent/FR2465080B1/fr
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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00—Stators
    • F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR7923489A 1979-09-17 1979-09-17 Dispositif de suspension aval de chambre de combustion pour turbomachines Granted FR2465080A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7923489A FR2465080A1 (fr) 1979-09-17 1979-09-17 Dispositif de suspension aval de chambre de combustion pour turbomachines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7923489A FR2465080A1 (fr) 1979-09-17 1979-09-17 Dispositif de suspension aval de chambre de combustion pour turbomachines

Publications (2)

Publication Number Publication Date
FR2465080A1 FR2465080A1 (fr) 1981-03-20
FR2465080B1 true FR2465080B1 (enExample) 1983-03-11

Family

ID=9229853

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7923489A Granted FR2465080A1 (fr) 1979-09-17 1979-09-17 Dispositif de suspension aval de chambre de combustion pour turbomachines

Country Status (1)

Country Link
FR (1) FR2465080A1 (enExample)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4597258A (en) * 1984-11-26 1986-07-01 United Technologies Corporation Combustor mount
DE4223733C2 (de) * 1992-07-18 1995-05-18 Gutehoffnungshuette Man Verbindung von Mischrohr und Flammrohr einer Gasturbine
US7493771B2 (en) * 2005-11-30 2009-02-24 General Electric Company Methods and apparatuses for assembling a gas turbine engine
US7637110B2 (en) 2005-11-30 2009-12-29 General Electric Company Methods and apparatuses for assembling a gas turbine engine
FR3096115B1 (fr) * 2019-05-14 2022-12-09 Safran Aircraft Engines Fixation de chambre de combustion de turbomachine
RU206240U1 (ru) * 2020-12-10 2021-09-01 Публичное Акционерное Общество "Одк-Сатурн" Узел соединения стенки жаровой трубы камеры сгорания и соплового аппарата газотурбинного двигателя

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1231258A (enExample) * 1960-09-28
FR709066A (fr) * 1930-01-24 1931-08-03 Asea Ab Dispositif perfectionné de montage d'une enveloppe intérieure dans une enveloppe extérieure
US2807934A (en) * 1951-12-06 1957-10-01 A V Roe Canada Ltd Flame tube support for a gas turbine combustion system
FR1248821A (fr) * 1960-02-17 1960-12-23 Entwicklungsbau Pirna Veb Chambre de combustion annulaire pour turbines à gaz, notamment pour avions et turbine équipée de ladite chambre ou d'une chambre similaire
GB1293555A (en) * 1969-03-28 1972-10-18 Lucas Industries Ltd Annular flame tube mounting for a gas turbine engine
GB1308452A (en) * 1969-03-28 1973-02-21 Lucas Industries Ltd Annular flame tube mounting for a gas turbine engine
US3759038A (en) * 1971-12-09 1973-09-18 Westinghouse Electric Corp Self aligning combustor and transition structure for a gas turbine
FR2278926A1 (fr) * 1974-07-19 1976-02-13 Creusot Loire Dispositif de positionnement relatif de deux enveloppes cylindriques coaxiales
US3905192A (en) * 1974-08-29 1975-09-16 United Aircraft Corp Combustor having staged premixing tubes
GB1539035A (en) * 1976-04-22 1979-01-24 Rolls Royce Combustion chambers for gas turbine engines

Also Published As

Publication number Publication date
FR2465080A1 (fr) 1981-03-20

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Legal Events

Date Code Title Description
CL Concession to grant licenses
ST Notification of lapse