CH643050A5 - Gasturbinentriebwerk mit ringbrennkammer. - Google Patents

Gasturbinentriebwerk mit ringbrennkammer. Download PDF

Info

Publication number
CH643050A5
CH643050A5 CH883279A CH883279A CH643050A5 CH 643050 A5 CH643050 A5 CH 643050A5 CH 883279 A CH883279 A CH 883279A CH 883279 A CH883279 A CH 883279A CH 643050 A5 CH643050 A5 CH 643050A5
Authority
CH
Switzerland
Prior art keywords
combustion chamber
section
sections
longitudinal
ring
Prior art date
Application number
CH883279A
Other languages
German (de)
English (en)
Inventor
Andrei Leonidovich Kuznetsov
Anatoly Vladimirovich Sudarev
Viktor Vasilievich Ivakhnenko
Jury Alexandrovich Lamm
Vladimir Alexeevich Maev
Jury Ivanovich Zakharov
Original Assignee
Proizv Ob Nevsky Z Im V I
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 Proizv Ob Nevsky Z Im V I filed Critical Proizv Ob Nevsky Z Im V I
Priority to CH883279A priority Critical patent/CH643050A5/de
Priority to US06/081,369 priority patent/US4302932A/en
Priority to FR7926406A priority patent/FR2468073A1/fr
Publication of CH643050A5 publication Critical patent/CH643050A5/de

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)
CH883279A 1979-10-01 1979-10-01 Gasturbinentriebwerk mit ringbrennkammer. CH643050A5 (de)

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 (1)

Publication Number Publication Date
CH643050A5 true CH643050A5 (de) 1984-05-15

Family

ID=27176080

Family Applications (1)

Application Number Title Priority Date Filing Date
CH883279A CH643050A5 (de) 1979-10-01 1979-10-01 Gasturbinentriebwerk mit ringbrennkammer.

Country Status (3)

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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110926823A (zh) * 2019-12-05 2020-03-27 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

Families Citing this family (11)

* 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

Family Cites Families (11)

* 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
FR1058665A (fr) * 1951-06-25 1954-03-18 Parsons C A & Co Ltd Perfectionnements apportés aux groupes moto-propulseurs comportant une turbine à gaz
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
BE535497A (enExample) * 1954-02-26
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
US3722215A (en) * 1971-03-30 1973-03-27 A Polyakov Gas-turbine plant
DE2140401C3 (de) * 1971-08-12 1979-12-06 Lucas Industries Ltd., Birmingham (Grossbritannien) Flammrohr für Gasturbinen

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110926823A (zh) * 2019-12-05 2020-03-27 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
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

Also Published As

Publication number Publication date
FR2468073A1 (fr) 1981-04-30
FR2468073B1 (enExample) 1983-07-08
US4302932A (en) 1981-12-01

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