FIELD: engines and pumps.
SUBSTANCE: claimed pilot burner comprises front body extending along burner central axis. Central axis is directed axially towards gas turbine engine combustion chamber. Said front body has front surface of pilot burner directed to combustion zone. Material is deposited/evaporated on front body to build up a heat-resistant body in axial direction of front body to make the pilot burner heat-resistant front surface. Said applied metal or alloy material resists the temperatures over 1000°C, particularly, those of up to 1500°C or higher.
EFFECT: longer life.
16 cl, 4 dwg
| Title |
Year |
Author |
Number |
| GAS TURBINE ENGINE PART WITH ANNULAR FIN AND GAS TURBINE ENGINE |
2006 |
|
RU2451187C2 |
| GAS TURBINE ENGINE COMPONENT, GAS TURBINE ENGINE WITH SID COMPONENT, METHOD OF PRODUCING LABYRINTH SEAL CIRCULAR KNIFE EDGE |
2006 |
|
RU2454547C2 |
| GAS TURBINE COMPONENT, GAS TURBINE ENGINE, METHOD OF MANUFACTURING GAS TURBINE ENGINE COMPONENT |
2015 |
- Subramanian, Ramesh
- Lampenscherf, Stefan
- Schillig, Cora
- Hitchman, Neil
- Zois, Dimitrios
|
RU2662003C2 |
| METHOD TO MANUFACTURE LABYRINTH SEAL COMB, THERMOMECHANICAL PART AND GAS TURBINE ENGINE COMPRISING SUCH COMB |
2006 |
|
RU2447342C2 |
| GAS TURBINE ENGINE ROTOR |
2008 |
|
RU2468210C2 |
| COMBUSTION CHAMBER AND GAS TURBINE ENGINE COMPRISING SUCH COMBUSTION CHAMBER |
2019 |
- Tsukidate, Khironori
- Oga, Kunikhiro
- Terada, Jositaka
- Nisida, Koiti
|
RU2738248C1 |
| GAS TURBINE ENGINE |
2013 |
- Batt Stefen
- Blak Richard
- Batler Devid
|
RU2616743C2 |
| GAS-TURBINE ENGINE |
2002 |
- Il'In Nikolaj Nikolaevich
|
RU2289028C2 |
| STATOR OF GAS TURBINE ENGINE TURBINE AND GAS TURBINE ENGINE |
2007 |
|
RU2449131C2 |
| GAS TURBINE ENGINE TURBINE |
2012 |
- Bolotin Nikolaj Borisovich
|
RU2500894C1 |
