FIELD: liquid fuel burning. SUBSTANCE: burner has water main line 9 with water pump 10, evaporator 12 in form of hermetically sealed heat-insulated reservoir accommodating tubular electric heater 13, check valve 11 at inlet of evaporator 12, starting valve 14 at outlet of evaporator 12, turbine 15. Nozzle assembly of turbine is connected with starting valve 14. Shafts of turbine 15, fan 2, fuel pump 5 and water pump 10 are kinematically connected. EFFECT: enlarged operating capabilities. 1 dwg
Title | Year | Author | Number |
---|---|---|---|
OIL/GAS COMBINATION BURNER | 1990 |
|
RU2013700C1 |
METHOD AND DEVICE FOR BURNING FUEL OIL | 1991 |
|
RU2013694C1 |
METHOD AND DEVICE FOR FEEDING MAZUT | 1991 |
|
RU2009398C1 |
FUEL OIL BURNER | 2010 |
|
RU2443942C1 |
SYSTEM FOR SUPPLYING HOT FUEL OIL TO BURNER | 0 |
|
SU1714297A1 |
PACKAGED BURNER | 2012 |
|
RU2494312C1 |
LIQUID ROCKET ENGINE | 1992 |
|
RU2040703C1 |
AIR THERMOSTATIC CONTROL OF SPACE VEHICLES | 1998 |
|
RU2135910C1 |
HOT-OIL FEEDING SYSTEM FOR BURNER | 0 |
|
SU1813991A1 |
BURNER NOZZLE | 2014 |
|
RU2564482C1 |
Authors
Dates
1994-04-30—Published
1991-03-28—Filed