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
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)
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)
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)
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)
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 |
-
1948
- 1948-11-30 FR FR1011066D patent/FR1011066A/en not_active Expired
-
1949
- 1949-11-26 CH CH296122D patent/CH296122A/en unknown
- 1949-11-29 GB GB30660/49A patent/GB686908A/en not_active Expired
- 1949-12-01 DE DES878A patent/DE944690C/en not_active Expired
-
1957
- 1957-01-30 FR FR71391D patent/FR71391E/en not_active Expired
- 1957-04-16 DE DES53169A patent/DE1084087B/en active Pending
Cited By (2)
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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