IT1139889B - Ugello del combustibile a duplice orifizio per motori a turbina a gas - Google Patents
Ugello del combustibile a duplice orifizio per motori a turbina a gasInfo
- Publication number
- IT1139889B IT1139889B IT25388/81A IT2538881A IT1139889B IT 1139889 B IT1139889 B IT 1139889B IT 25388/81 A IT25388/81 A IT 25388/81A IT 2538881 A IT2538881 A IT 2538881A IT 1139889 B IT1139889 B IT 1139889B
- Authority
- IT
- Italy
- Prior art keywords
- gas turbine
- fuel nozzle
- turbine engines
- double orifice
- orifice fuel
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/36—Details
- F23D11/38—Nozzles; Cleaning devices therefor
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Nozzles For Spraying Of Liquid Fuel (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US06/212,175 US4395874A (en) | 1980-12-02 | 1980-12-02 | Fuel nozzles with water injection for gas turbine engines |
| US06/212,176 US4418543A (en) | 1980-12-02 | 1980-12-02 | Fuel nozzle for gas turbine engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| IT8125388A0 IT8125388A0 (it) | 1981-12-02 |
| IT1139889B true IT1139889B (it) | 1986-09-24 |
Family
ID=26906850
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| IT25388/81A IT1139889B (it) | 1980-12-02 | 1981-12-02 | Ugello del combustibile a duplice orifizio per motori a turbina a gas |
Country Status (6)
| Country | Link |
|---|---|
| DE (1) | DE3147564A1 (cs) |
| FR (1) | FR2495229B1 (cs) |
| GB (1) | GB2091410B (cs) |
| IL (1) | IL64422A (cs) |
| IT (1) | IT1139889B (cs) |
| SE (1) | SE456601B (cs) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3642122C1 (de) * | 1986-12-10 | 1988-06-09 | Mtu Muenchen Gmbh | Brennstoffeinspritzvorrichtung |
| DE19860785A1 (de) * | 1998-12-30 | 2000-07-06 | Abb Alstom Power Ch Ag | Zerstäubungsvorrichtung |
| RU2212588C1 (ru) * | 2002-03-22 | 2003-09-20 | Акционерное общество открытого типа Авиамоторный научно-технический комплекс "Союз" | Горелочное устройство камеры сгорания авиационного газотурбинного двигателя |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2965303A (en) * | 1959-03-30 | 1960-12-20 | United Aircraft Corp | Coolant injection in a fuel nozzle |
| GB1114728A (en) * | 1967-03-20 | 1968-05-22 | Rolls Royce | Burner e.g. for a gas turbine engine combustion chamber |
| DE2012941A1 (de) * | 1969-04-01 | 1970-10-15 | Parker-Hannifin Corp., Cleveland, Ohio (V.St.A.) | Einspritzdüse für flüssigen Kraftstoff |
| US3684186A (en) * | 1970-06-26 | 1972-08-15 | Ex Cell O Corp | Aerating fuel nozzle |
| GB1377184A (en) * | 1971-02-02 | 1974-12-11 | Secr Defence | Gas turbine engine combustion apparatus |
| US3768250A (en) * | 1971-12-01 | 1973-10-30 | Mitsubishi Heavy Ind Ltd | Combustion apparatus for a gas turbine |
| JPS5342897B2 (cs) * | 1972-11-09 | 1978-11-15 | ||
| GB1421399A (en) * | 1972-11-13 | 1976-01-14 | Snecma | Fuel injectors |
| FR2249243B2 (cs) * | 1973-10-26 | 1978-09-15 | Snecma | |
| FR2206796A5 (cs) * | 1972-11-13 | 1974-06-07 | Snecma | |
| US3866413A (en) * | 1973-01-22 | 1975-02-18 | Parker Hannifin Corp | Air blast fuel atomizer |
| US3979069A (en) * | 1974-10-11 | 1976-09-07 | Luigi Garofalo | Air-atomizing fuel nozzle |
| US4139157A (en) * | 1976-09-02 | 1979-02-13 | Parker-Hannifin Corporation | Dual air-blast fuel nozzle |
| US4290558A (en) * | 1979-09-18 | 1981-09-22 | United Technologies Corporation | Fuel nozzle with water injection |
-
1981
- 1981-12-01 GB GB8136226A patent/GB2091410B/en not_active Expired
- 1981-12-01 SE SE8107164A patent/SE456601B/sv not_active IP Right Cessation
- 1981-12-01 IL IL64422A patent/IL64422A/xx not_active IP Right Cessation
- 1981-12-01 FR FR8122490A patent/FR2495229B1/fr not_active Expired
- 1981-12-01 DE DE19813147564 patent/DE3147564A1/de active Granted
- 1981-12-02 IT IT25388/81A patent/IT1139889B/it active
Also Published As
| Publication number | Publication date |
|---|---|
| SE8107164L (sv) | 1982-06-03 |
| GB2091410A (en) | 1982-07-28 |
| IL64422A0 (en) | 1982-03-31 |
| IL64422A (en) | 1986-09-30 |
| SE456601B (sv) | 1988-10-17 |
| IT8125388A0 (it) | 1981-12-02 |
| FR2495229B1 (fr) | 1987-07-03 |
| GB2091410B (en) | 1984-08-22 |
| DE3147564A1 (de) | 1982-08-19 |
| DE3147564C2 (cs) | 1991-07-11 |
| FR2495229A1 (fr) | 1982-06-04 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| IT1087034B (it) | Ugello del combustibile per turbine a gas | |
| GB2073401B (en) | Fuel nozzle guide heatshield for a gas turbine engine | |
| GB2073398B (en) | Fuel nozzle guide and seal for a gas turbine engine | |
| IT7824303A0 (it) | Perfezionamenti apportati ai bruciatori di combustibile per motori a turbina a gas. | |
| DE3265642D1 (en) | Fuel nozzle assembly for a gas turbine engine | |
| JPS5720539A (en) | Exhaust nozzle for gas turbine engine | |
| IT7822829A0 (it) | Struttura a paletta di guida per ugelli di motori a turbina a gas. | |
| IT7828914A0 (it) | Perfezionamenti apportati ai dispositivi di combustione per motori a turbina a gas. | |
| IT1132128B (it) | Valvola di distribuzione del combustibile per un motore a turbina a gas | |
| GB2004050B (en) | Fuel nozzle assembly for a gas turbine engine | |
| JPS51146613A (en) | Variable area nozzle for gas turbine engine | |
| IL62269A (en) | Anti-coke nozzle for gas turbine combustor | |
| IT7921209A0 (it) | Perfezionamenti apportati alle palette direttrici per motori a turbina a gas. | |
| IT1213558B (it) | Valvola dosatrice del combustibile per motori a turbina a gas. | |
| GB1553701A (en) | Nozzle guide vane for a gas turbine engine | |
| IT8020740A0 (it) | Perfezionamenti apportati ai bruciatori per motori a turbina agas. | |
| IT7919648A0 (it) | Motori a turbina a gas. | |
| GB2107405B (en) | Nozzle guide vane for a gas turbine engine | |
| IT1065037B (it) | Ugello d'iniezione per il carburante in macchine a combustione,in paricolare per turbine a gas | |
| IT1139889B (it) | Ugello del combustibile a duplice orifizio per motori a turbina a gas | |
| IL63171A0 (en) | Fuel nozzle for a gas turbine engine | |
| IT1115456B (it) | Perfezionamenti in ugelli per motori a turbina a gas | |
| GB2367592B (en) | Thrust nozzle for a gas turbine engine | |
| IT1139469B (it) | Impianto ed apparato di controllo del carburante per motori a turbina a gas | |
| JPS5537591A (en) | Assembly of jet pipe with variableearea final nozzle for gas turbine engine |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| TA | Fee payment date (situation as of event date), data collected since 19931001 |
Effective date: 19971129 |