CH262382A - Verbrennungsturbinenanlage. - Google Patents
Verbrennungsturbinenanlage.Info
- Publication number
- CH262382A CH262382A CH262382DA CH262382A CH 262382 A CH262382 A CH 262382A CH 262382D A CH262382D A CH 262382DA CH 262382 A CH262382 A CH 262382A
- Authority
- CH
- Switzerland
- Prior art keywords
- turbine plant
- combustion turbine
- combustion
- plant
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB262382X | 1944-11-28 |
Publications (1)
Publication Number | Publication Date |
---|---|
CH262382A true CH262382A (de) | 1949-06-30 |
Family
ID=10240490
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CH262382D CH262382A (de) | 1944-11-28 | 1946-09-05 | Verbrennungsturbinenanlage. |
Country Status (5)
Country | Link |
---|---|
BE (1) | BE468998A (fr) |
CH (1) | CH262382A (fr) |
FR (1) | FR943200A (fr) |
GB (1) | GB588847A (fr) |
NL (1) | NL67338C (fr) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0030880B1 (fr) * | 1979-12-13 | 1983-08-31 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." | Dispositif d'injection pour chambre à combustion de moteur à turbine |
CH666340A5 (en) * | 1985-05-29 | 1988-07-15 | Bbc Brown Boveri & Cie | Gas turbine combustion chamber - has fuel lines to burner nozzles extending through secondary air duct and contained in tubes connected to atmosphere |
EP0350503A1 (fr) * | 1987-12-14 | 1990-01-17 | Sundstrand Corp | Injecteurs de carburant pour moteurs a turbine. |
EP0577862A1 (fr) * | 1992-07-03 | 1994-01-12 | Abb Research Ltd. | Dispositif de post-combustion |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2648950A (en) * | 1949-08-24 | 1953-08-18 | Westinghouse Electric Corp | Gas turbine engine apparatus designed to burn wet pulverized fuel |
US3003316A (en) * | 1953-02-10 | 1961-10-10 | Rolls Royce | Cooling means for forked exhaust ducts of gas turbine engines |
US2861424A (en) * | 1954-04-09 | 1958-11-25 | Douglas Aircraft Co Inc | Fuel supply means for combustion apparatus |
US2944388A (en) * | 1955-02-24 | 1960-07-12 | Thompson Ramo Wooldridge Inc | Air atomizing spray bar |
US2942414A (en) * | 1956-07-03 | 1960-06-28 | Thompson Ramo Wooldridge Inc | Umbrella spraybar afterburner arrangement |
BE795529A (fr) * | 1972-02-17 | 1973-06-18 | Gen Electric | Allumeur monte sur un dispositif d'augmentation de la poussee de turboreacteurs et refroidi a l'air |
US4070826A (en) * | 1975-12-24 | 1978-01-31 | General Electric Company | Low pressure fuel injection system |
US4798048A (en) * | 1987-12-21 | 1989-01-17 | United Technologies Corporation | Augmentor pilot |
US4887425A (en) * | 1988-03-18 | 1989-12-19 | General Electric Company | Fuel spraybar |
US8869941B2 (en) * | 2009-11-16 | 2014-10-28 | Textron Innovations Inc. | Dual-path fluid injection jet |
US9638422B2 (en) * | 2012-06-22 | 2017-05-02 | Delavan Inc. | Active purge mechanism with backflow preventer for gas turbine fuel injectors |
WO2015054136A1 (fr) | 2013-10-07 | 2015-04-16 | United Technologies Corporation | Injecteur de carburant refroidi à l'air pour moteur à turbine |
EP3109550B1 (fr) | 2015-06-19 | 2019-09-04 | Rolls-Royce Corporation | Air de refroidissement refroidi de turbine circulant par un agencement tubulaire |
-
0
- BE BE468998D patent/BE468998A/xx unknown
- NL NL67338D patent/NL67338C/xx active
-
1944
- 1944-11-28 GB GB23752/44A patent/GB588847A/en not_active Expired
-
1946
- 1946-08-28 FR FR943200D patent/FR943200A/fr not_active Expired
- 1946-09-05 CH CH262382D patent/CH262382A/de unknown
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0030880B1 (fr) * | 1979-12-13 | 1983-08-31 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." | Dispositif d'injection pour chambre à combustion de moteur à turbine |
CH666340A5 (en) * | 1985-05-29 | 1988-07-15 | Bbc Brown Boveri & Cie | Gas turbine combustion chamber - has fuel lines to burner nozzles extending through secondary air duct and contained in tubes connected to atmosphere |
EP0350503A1 (fr) * | 1987-12-14 | 1990-01-17 | Sundstrand Corp | Injecteurs de carburant pour moteurs a turbine. |
EP0350503A4 (fr) * | 1987-12-14 | 1990-05-14 | Sundstrand Corp | Injecteurs de carburant pour moteurs a turbine. |
EP0577862A1 (fr) * | 1992-07-03 | 1994-01-12 | Abb Research Ltd. | Dispositif de post-combustion |
US5431018A (en) * | 1992-07-03 | 1995-07-11 | Abb Research Ltd. | Secondary burner having a through-flow helmholtz resonator |
Also Published As
Publication number | Publication date |
---|---|
BE468998A (fr) | |
GB588847A (en) | 1947-06-04 |
FR943200A (fr) | 1949-03-01 |
NL67338C (fr) |
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