FIELD: machine building.
SUBSTANCE: disclosed is fuel injector (600) for gas turbine engine. Fuel injector (600) comprises two primary tubes, secondary tube (603), a primary passage for gas and a secondary passage for gas. Two primary tubes are connected in parallel to supply the main gaseous fuel into the primary passage for gas. Secondary pipe (603) supplies main gaseous fuel to secondary gas passage independent of two primary tubes and primary gas passage.
EFFECT: primary passage for gas and secondary passage for gas supply main gaseous fuel into channel for preliminary mixing, independently providing reliable control of gas turbine engine.
10 cl, 13 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| FUEL INJECTOR WITH GAS DISTRIBUTION THROUGH PLURALITY OF TUBES | 2016 |
|
RU2721627C2 |
| FUEL INJECTOR WITH CENTER BODY ASSEMBLY | 2019 |
|
RU2790900C2 |
| FUEL INJECTOR AND FUEL SYSTEM FOR INTERNAL COMBUSTION ENGINE | 2017 |
|
RU2726451C2 |
| SHROUDED PILOT LIQUID TUBE | 2014 |
|
RU2657075C2 |
| FUEL INJECTOR OF GAS TURBINE ENGINE WITH REMOVABLE AUXILIARY LIQUID FUEL PIPE | 2008 |
|
RU2468296C2 |
| INNER PREMIX TUBE AIR WIPE | 2014 |
|
RU2657072C2 |
| OUTER PREMIX BARREL VENT AIR SWEEP | 2014 |
|
RU2657080C2 |
| SWIRLER, COMBUSTION CHAMBER UNIT AND GAS TURBINE WITH IMPROVED FUEL/AIR MIXING | 2017 |
|
RU2715129C1 |
| TAPERED GAS TURBINE ENGINE LIQUID GALLERY | 2014 |
|
RU2664904C2 |
| HEAT-INSULATED FUEL ATOMISER FOR GAS TURBINE ENGINE | 2015 |
|
RU2696158C2 |
