CH345203A - Gasturbinentriebwerk mit Kompressor und ringförmiger Verbrennungskammer - Google Patents
Gasturbinentriebwerk mit Kompressor und ringförmiger VerbrennungskammerInfo
- Publication number
- CH345203A CH345203A CH345203DA CH345203A CH 345203 A CH345203 A CH 345203A CH 345203D A CH345203D A CH 345203DA CH 345203 A CH345203 A CH 345203A
- Authority
- CH
- Switzerland
- Prior art keywords
- compressor
- combustion chamber
- gas turbine
- turbine engine
- annular combustion
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 title 1
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
- F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
- F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
-
- 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
- F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices
- F23R3/32—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising devices being tubular
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)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB345203X | 1955-03-16 | ||
GB80356X | 1956-03-08 |
Publications (1)
Publication Number | Publication Date |
---|---|
CH345203A true CH345203A (de) | 1960-03-15 |
Family
ID=26241850
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH345203D CH345203A (de) | 1955-03-16 | 1956-03-16 | Gasturbinentriebwerk mit Kompressor und ringförmiger Verbrennungskammer |
Country Status (5)
Country | Link |
---|---|
US (1) | US2977760A (de) |
CH (1) | CH345203A (de) |
DE (1) | DE1045727B (de) |
FR (1) | FR1150175A (de) |
GB (1) | GB798474A (de) |
Families Citing this family (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL251000A (de) * | 1959-04-28 | |||
US3203180A (en) * | 1960-03-16 | 1965-08-31 | Nathan C Price | Turbo-jet powerplant |
GB903834A (en) * | 1960-05-18 | 1962-08-22 | Rolls Royce | Combustion chamber |
DE1164159B (de) * | 1961-04-19 | 1964-02-27 | Bristol Siddeley Engines Ltd | Brennkammer fuer Gasturbinentriebwerke |
GB943250A (en) * | 1962-02-01 | 1963-12-04 | Rolls Royce | Improvements in or relating to gas turbine combustion chambers |
GB1035541A (en) * | 1964-02-21 | 1966-07-13 | Rolls Royce | Combustion equipment for a gas turbine engine |
GB1017900A (en) * | 1964-12-02 | 1966-01-26 | Rolls Royce | Combustion chambers |
US3579983A (en) * | 1969-05-05 | 1971-05-25 | Snecma | Improvements in or relating to combustion chambers |
US3701255A (en) * | 1970-10-26 | 1972-10-31 | United Aircraft Corp | Shortened afterburner construction for turbine engine |
US3675419A (en) * | 1970-10-26 | 1972-07-11 | United Aircraft Corp | Combustion chamber having swirling flow |
GB1443431A (en) * | 1972-12-16 | 1976-07-21 | Rolls Royce | Seal between relatively moving components of a fluid flow machine |
US4117669A (en) * | 1977-03-04 | 1978-10-03 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Apparatus and method for reducing thermal stress in a turbine rotor |
FR2410138A2 (fr) * | 1977-11-29 | 1979-06-22 | Snecma | Perfectionnements aux chambres de combustion pour moteur a turbine a gaz |
GB2098719B (en) * | 1981-05-20 | 1984-11-21 | Rolls Royce | Gas turbine engine combustion apparatus |
US5058375A (en) * | 1988-12-28 | 1991-10-22 | Sundstrand Corporation | Gas turbine annular combustor with radial dilution air injection |
US5088287A (en) * | 1989-07-13 | 1992-02-18 | Sundstrand Corporation | Combustor for a turbine |
US5109671A (en) * | 1989-12-05 | 1992-05-05 | Allied-Signal Inc. | Combustion apparatus and method for a turbine engine |
US6453676B1 (en) * | 2000-06-29 | 2002-09-24 | Industrial Technology Research Institute | 50 pound thrust level turbojet engine |
US6536201B2 (en) * | 2000-12-11 | 2003-03-25 | Pratt & Whitney Canada Corp. | Combustor turbine successive dual cooling |
US10151243B2 (en) * | 2013-02-23 | 2018-12-11 | Rolls-Royce Corporation | Cooled cooling air taken directly from combustor dome |
CN114719292A (zh) * | 2022-03-15 | 2022-07-08 | 西北工业大学 | 一种微型燃烧室燃油对流雾化方案 |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2243467A (en) * | 1937-02-13 | 1941-05-27 | Jendrassik George | Process and equipment for gas turbines |
DE866878C (de) * | 1944-07-13 | 1953-02-12 | E H Dr Phil H C Ernst Heinkel | Ringbrennkammer fuer Gasturbinen |
DE826805C (de) * | 1944-11-11 | 1952-01-07 | Maschf Augsburg Nuernberg Ag | Gasturbinenanlage |
DE847530C (de) * | 1944-11-17 | 1952-08-25 | Hellmut Weinrich | Ringfoermige Brennkammer, insbesondere fuer Gasturbinen |
US2503006A (en) * | 1945-04-24 | 1950-04-04 | Edward A Stalker | Gas turbine engine with controllable auxiliary jet |
GB652991A (en) * | 1947-02-28 | 1951-05-09 | Lysholm Alf | Gas turbine power plant |
GB666062A (en) * | 1947-02-28 | 1952-02-06 | Lysholm Alf | Gas turbine power plant |
US2603949A (en) * | 1947-11-28 | 1952-07-22 | United Aircraft Corp | Combustion chamber with diverse air paths and vortices producing vanes therein for jet propulsion or gas turbine power plants |
FR967324A (fr) * | 1948-05-31 | 1950-10-31 | Turbo-machines | |
US2541900A (en) * | 1948-12-24 | 1951-02-13 | A V Roe Canada Ltd | Multiple fuel jet burner and torch igniter unit with fuel vaporizing tubes |
GB702273A (en) * | 1949-05-18 | 1954-01-13 | Lysholm Alf | Improvements in or relating to gas turbine power plants |
US2775864A (en) * | 1951-04-10 | 1957-01-01 | Gen Motors Corp | Jet propulsion engine with afterburner |
-
1955
- 1955-03-16 GB GB7716/55A patent/GB798474A/en not_active Expired
-
1956
- 1956-03-12 US US571049A patent/US2977760A/en not_active Expired - Lifetime
- 1956-03-14 DE DEB39512A patent/DE1045727B/de active Pending
- 1956-03-16 FR FR1150175D patent/FR1150175A/fr not_active Expired
- 1956-03-16 CH CH345203D patent/CH345203A/de unknown
Also Published As
Publication number | Publication date |
---|---|
US2977760A (en) | 1961-04-04 |
DE1045727B (de) | 1958-12-04 |
FR1150175A (fr) | 1958-01-08 |
GB798474A (en) | 1958-07-23 |
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