FR2468073A1 - Chambre de combustion annulaire de turbomoteur - Google Patents

Chambre de combustion annulaire de turbomoteur Download PDF

Info

Publication number
FR2468073A1
FR2468073A1 FR7926406A FR7926406A FR2468073A1 FR 2468073 A1 FR2468073 A1 FR 2468073A1 FR 7926406 A FR7926406 A FR 7926406A FR 7926406 A FR7926406 A FR 7926406A FR 2468073 A1 FR2468073 A1 FR 2468073A1
Authority
FR
France
Prior art keywords
combustion chamber
annular
sections
ferrules
section
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.)
Granted
Application number
FR7926406A
Other languages
English (en)
French (fr)
Other versions
FR2468073B1 (enExample
Inventor
Andrei Leonidovich Kuznetsov
Anatoly Vladimirovich Sudarev
Viktor Vasilievich Ivakhnenko
Jury Alexandrovich Lamm
Vladimir Alexeevich Maev
Jury Ivanovich Zakharov
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.)
PROIZV OBIEDINE NEVSKY
Original Assignee
PROIZV OBIEDINE NEVSKY
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
Priority to CH883279A priority Critical patent/CH643050A5/de
Priority to US06/081,369 priority patent/US4302932A/en
Application filed by PROIZV OBIEDINE NEVSKY filed Critical PROIZV OBIEDINE NEVSKY
Priority to FR7926406A priority patent/FR2468073A1/fr
Publication of FR2468073A1 publication Critical patent/FR2468073A1/fr
Application granted granted Critical
Publication of FR2468073B1 publication Critical patent/FR2468073B1/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
    • F23R3/002—Wall structures
    • 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
    • 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

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)
FR7926406A 1979-10-01 1979-10-24 Chambre de combustion annulaire de turbomoteur Granted FR2468073A1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
CH883279A CH643050A5 (de) 1979-10-01 1979-10-01 Gasturbinentriebwerk mit ringbrennkammer.
US06/081,369 US4302932A (en) 1979-10-01 1979-10-03 Annular combustor of gas turbine engine
FR7926406A FR2468073A1 (fr) 1979-10-01 1979-10-24 Chambre de combustion annulaire de turbomoteur

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
CH883279A CH643050A5 (de) 1979-10-01 1979-10-01 Gasturbinentriebwerk mit ringbrennkammer.
US06/081,369 US4302932A (en) 1979-10-01 1979-10-03 Annular combustor of gas turbine engine
FR7926406A FR2468073A1 (fr) 1979-10-01 1979-10-24 Chambre de combustion annulaire de turbomoteur

Publications (2)

Publication Number Publication Date
FR2468073A1 true FR2468073A1 (fr) 1981-04-30
FR2468073B1 FR2468073B1 (enExample) 1983-07-08

Family

ID=27176080

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7926406A Granted FR2468073A1 (fr) 1979-10-01 1979-10-24 Chambre de combustion annulaire de turbomoteur

Country Status (3)

Country Link
US (1) US4302932A (enExample)
CH (1) CH643050A5 (enExample)
FR (1) FR2468073A1 (enExample)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4413470A (en) * 1981-03-05 1983-11-08 Electric Power Research Institute, Inc. Catalytic combustion system for a stationary combustion turbine having a transition duct mounted catalytic element
US4471623A (en) * 1982-10-15 1984-09-18 The United States Of America As Represented By The Secretary Of The Air Force Combustion chamber floatwall panel attachment arrangement
GB2135440B (en) * 1983-02-19 1986-06-25 Rolls Royce Mounting combustion chambers
US4944151A (en) * 1988-09-26 1990-07-31 Avco Corporation Segmented combustor panel
FR2652858B1 (fr) * 1989-10-11 1993-05-07 Snecma Stator de turbomachine associe a des moyens de deformation.
US5323604A (en) * 1992-11-16 1994-06-28 General Electric Company Triple annular combustor for gas turbine engine
US5289685A (en) * 1992-11-16 1994-03-01 General Electric Company Fuel supply system for a gas turbine engine
US5303542A (en) * 1992-11-16 1994-04-19 General Electric Company Fuel supply control method for a gas turbine engine
GB2420614B (en) * 2004-11-30 2009-06-03 Alstom Technology Ltd Tile and exo-skeleton tile structure
RU2310086C1 (ru) * 2006-02-13 2007-11-10 Закрытое Акционерное общество "Научно-Производственная Фирма "НЕВТУРБОТЕСТ" (ЗАО НПФ "НЕВТУРБОТЕСТ") Газотурбинная установка
US10801731B2 (en) * 2018-09-13 2020-10-13 United Technologies Corporation Attachment for high temperature CMC combustor panels
CN110926823B (zh) * 2019-12-05 2021-08-20 中国航发四川燃气涡轮研究院 一种高压舱式主燃烧室扇形试验件结构

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1058665A (fr) * 1951-06-25 1954-03-18 Parsons C A & Co Ltd Perfectionnements apportés aux groupes moto-propulseurs comportant une turbine à gaz
FR1122030A (fr) * 1954-02-26 1956-08-30 Rolls Royce Perfectionnements aux parois réfractaires
GB791051A (en) * 1954-07-30 1958-02-19 Power Jets Res & Dev Ltd Improvements in combustion chambers
GB846317A (en) * 1957-10-31 1960-08-31 Lucas Industries Ltd Liquid fuel combustion apparatus
US3031844A (en) * 1960-08-12 1962-05-01 William A Tomolonius Split combustion liner
US3398527A (en) * 1966-05-31 1968-08-27 Air Force Usa Corrugated wall radiation cooled combustion chamber
DE2140401A1 (de) * 1971-08-12 1973-03-01 Lucas Industries Ltd Flammrohr fuer gasturbinen

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2544538A (en) * 1948-12-01 1951-03-06 Wright Aeronautical Corp Liner for hot gas chambers
US2710523A (en) * 1951-09-27 1955-06-14 A V Roe Canada Ltd Gas turbine tail cone
US2760338A (en) * 1952-02-02 1956-08-28 A V Roe Canada Ltd Annular combustion chamber for gas turbine engine
US3722215A (en) * 1971-03-30 1973-03-27 A Polyakov Gas-turbine plant

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1058665A (fr) * 1951-06-25 1954-03-18 Parsons C A & Co Ltd Perfectionnements apportés aux groupes moto-propulseurs comportant une turbine à gaz
FR1122030A (fr) * 1954-02-26 1956-08-30 Rolls Royce Perfectionnements aux parois réfractaires
GB791051A (en) * 1954-07-30 1958-02-19 Power Jets Res & Dev Ltd Improvements in combustion chambers
GB846317A (en) * 1957-10-31 1960-08-31 Lucas Industries Ltd Liquid fuel combustion apparatus
US3031844A (en) * 1960-08-12 1962-05-01 William A Tomolonius Split combustion liner
US3398527A (en) * 1966-05-31 1968-08-27 Air Force Usa Corrugated wall radiation cooled combustion chamber
DE2140401A1 (de) * 1971-08-12 1973-03-01 Lucas Industries Ltd Flammrohr fuer gasturbinen

Also Published As

Publication number Publication date
CH643050A5 (de) 1984-05-15
FR2468073B1 (enExample) 1983-07-08
US4302932A (en) 1981-12-01

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