FIELD: aircraft engineering.
SUBSTANCE: increase in hydrocarbon fuel combustion efficiency consists in pumping the fuel from fuelling tank in variable homogeneous electric field for 30-40 minutes into extra tank. Therefrom fuel is forced directly before aircraft takeoff into aircraft engine tank and, further, via pressure fuel line to the nozzle.
EFFECT: better tip leakage parameters at fuel nozzle outlet, attainment of fine fuel-air mix.
3 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF INCREASING EFFICIENCY OF FUEL SPRAY | 2014 |
|
RU2582376C1 |
| METHOD OF EFFICIENCY INCREASING OF HYDROCARBON FUEL COMBUSTION | 2013 |
|
RU2562505C2 |
| FUEL JET OF GAS TURBINE ENGINE | 2015 |
|
RU2615618C1 |
| FUEL JET OF AIRCRAFT ENGINE | 2016 |
|
RU2636947C1 |
| FUEL NOZZLE | 2016 |
|
RU2634649C1 |
| METHOD OF INTENSIFYING ICE OPERATION | 2007 |
|
RU2352806C1 |
| ICE WITH MAGNETIC-CATALYTIC COMBUSTION CHAMBER AND WITH ULTRASONIC STEAM GENERATOR AND METHOD FOR SUPPLY OF GAS-WATER-AIR FUEL MIXTURE TO COMBUSTION CHAMBER OF THIS ICE | 2019 |
|
RU2708180C1 |
| METHOD FOR SUPPLYING FUEL INTO INTERNAL COMBUSTION ENGINE (ICE) AND SYSTEM WITH STEAM GENERATOR FOR IMPLEMENTATION THEREOF | 2016 |
|
RU2681873C2 |
| OPERATING METHOD OF INTERNAL COMBUSTION ENGINE (ICE) WITH SPARK IGNITION AND FUEL SUPPLY DEVICE THEREFOR | 2019 |
|
RU2722006C1 |
| DEVICE FOR MAGNETOACOUSTIC TREATMENT OF LIQUID HYDROCARBON FUEL | 2013 |
|
RU2546886C1 |
