CH296122A - Gas turbine installation. - Google Patents

Gas turbine installation.

Info

Publication number
CH296122A
CH296122A CH296122DA CH296122A CH 296122 A CH296122 A CH 296122A CH 296122D A CH296122D A CH 296122DA CH 296122 A CH296122 A CH 296122A
Authority
CH
Switzerland
Prior art keywords
gas turbine
turbine installation
installation
gas
turbine
Prior art date
Application number
Other languages
French (fr)
Inventor
Szydlowski Joseph
Original Assignee
Szydlowski Joseph
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 Szydlowski Joseph filed Critical Szydlowski Joseph
Publication of CH296122A publication Critical patent/CH296122A/en

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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/38—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising rotary fuel injection means
    • 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
    • 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)
  • Sealing Using Fluids, Sealing Without Contact, And Removal Of Oil (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)
  • Pre-Mixing And Non-Premixing Gas Burner (AREA)
CH296122D 1948-11-30 1949-11-26 Gas turbine installation. CH296122A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR944690X 1948-11-30

Publications (1)

Publication Number Publication Date
CH296122A true CH296122A (en) 1954-01-31

Family

ID=9471874

Family Applications (1)

Application Number Title Priority Date Filing Date
CH296122D CH296122A (en) 1948-11-30 1949-11-26 Gas turbine installation.

Country Status (4)

Country Link
CH (1) CH296122A (en)
DE (2) DE944690C (en)
FR (2) FR1011066A (en)
GB (1) GB686908A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1055884B (en) * 1954-03-02 1959-04-23 Bristol Aero Engines Ltd Flame tube for a combustion chamber of a gas turbine engine
RU2506499C2 (en) * 2009-11-09 2014-02-10 Дженерал Электрик Компани Fuel atomisers of gas turbine with opposite swirling directions

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2882681A (en) * 1953-02-24 1959-04-21 Lucas Industries Ltd Air-jacketed annular combustion chambers for jet-propulsion engines, gas turbines or like prime movers
US3088281A (en) * 1956-04-03 1963-05-07 Bristol Siddeley Engines Ltd Combustion chambers for use with swirling combustion supporting medium
FR1164675A (en) * 1957-01-08 1958-10-13 Improvements to rotary injection devices for gas turbine combustion chambers
FR1166664A (en) * 1957-02-05 1958-11-13 Improvements to the combustion chambers which can be used, in particular, in reactors
NL108658C (en) * 1958-07-31
DE1179422B (en) * 1959-01-29 1964-10-08 Rolls Royce Combustion chamber, especially for jet engines
NL111857C (en) * 1959-04-28
DE1214053B (en) * 1960-09-14 1966-04-07 Snecma Turbine jet engine
DE1165936B (en) * 1961-01-21 1964-03-19 Gasturbinenbau Und Energiemasc Combustion chamber for gas turbines
DE1218800B (en) * 1961-04-25 1966-06-08 M A N Turbo Ges Mit Beschraenk Gas turbine, in particular small gas turbine
CH398182A (en) * 1962-11-14 1965-08-31 Saurer Ag Adolph Gas turbine plant
FR1424457A (en) * 1964-11-30 1966-01-14 Improvements made to the combustion chambers of gas turbine engines
DE1258663B (en) * 1965-12-02 1968-01-11 Stroemungsmasch Veb Gas turbine with annular combustion chamber
US5042256A (en) * 1986-07-28 1991-08-27 Teledyne Industries, Inc. Turbine shaft fuel pump
US5265409A (en) * 1992-12-18 1993-11-30 United Technologies Corporation Uniform cooling film replenishment thermal liner assembly
FR2708086B1 (en) * 1993-06-30 1995-09-01 Snecma Sectorized tubular structure working on implosion.
DE19846976A1 (en) * 1998-10-12 2000-04-13 Bmw Rolls Royce Gmbh Fuel injection system for radial or slinger combustion chamber of small gas turbine with radial or diagonal compressor located in front of combustion chamber to which is connected turbine part via axially running rotor shaft
US8640464B2 (en) 2009-02-23 2014-02-04 Williams International Co., L.L.C. Combustion system
CN114857621B (en) * 2022-05-07 2023-05-12 燕山大学 Atomizing jet nozzle device and atomizing method for high-pressure non-Newtonian fluid
CN115164236A (en) * 2022-06-15 2022-10-11 中科航星科技有限公司 Heat insulation assembly suitable for oil thrower disc combustion chamber

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE147825C (en) *
FR741858A (en) * 1932-07-30 1933-02-22
US2085761A (en) * 1933-02-15 1937-07-06 Milo Ab Aircraft power plant
CH188758A (en) * 1935-05-16 1937-01-15 Whittle Frank Power plant for propelling aircraft.
CH195823A (en) * 1936-03-04 1938-02-15 Frank Whittle Device for propelling aircraft by reaction.
FR866391A (en) * 1938-05-27 1941-08-04 Jet apparatus for gaseous agents, used in particular to produce the traction and the ascent of aircraft
GB585343A (en) * 1942-09-29 1947-02-05 Armstrong Siddeley Motors Ltd Combustion chambers of internal-combustion turbine plant
GB612532A (en) * 1946-04-08 1948-11-15 Adrian Albert Lombard Improvements in or relating to combustion chambers for internal combustion turbines
US2547619A (en) * 1948-11-27 1951-04-03 Gen Electric Combustor with sectional housing and liner
GB701099A (en) * 1950-05-22 1953-12-16 Lucas Ltd Joseph Improvements to combustion chambers
GB742657A (en) * 1953-01-16 1955-12-30 Rolls Royce Improvements in or relating to hot-gas-conveying ducting
GB756279A (en) * 1954-08-30 1956-09-05 Joseph Thompson Purvis Combustion chamber assembly for gas turbine engines

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1055884B (en) * 1954-03-02 1959-04-23 Bristol Aero Engines Ltd Flame tube for a combustion chamber of a gas turbine engine
RU2506499C2 (en) * 2009-11-09 2014-02-10 Дженерал Электрик Компани Fuel atomisers of gas turbine with opposite swirling directions

Also Published As

Publication number Publication date
FR71391E (en) 1959-12-22
DE1084087B (en) 1960-06-23
GB686908A (en) 1953-02-04
DE944690C (en) 1956-06-21
FR1011066A (en) 1952-06-18

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