FIELD: engines and pumps.
SUBSTANCE: in addition, in order to increase the power of an air starter, the air supplied to the air starter turbine is heated due to combustion of fuel in it, the dosing of which is performed depending on pressure and temperature of air at the air starter inlet and gas temperature in the heating zone.
EFFECT: increase of available power of the air starter and improvement of the gas turbine engine start-up reliability.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF STARTING GAS TURBINE ENGINE | 2011 |
|
RU2491437C2 |
| METHOD OF FUEL FLOW CONTROL AT START OF GAS TURBINE ENGINE | 2010 |
|
RU2435973C1 |
| GAS-TURBINE ENGINE FUEL SYSTEM | 2006 |
|
RU2317431C1 |
| METHOD TO CONTROL GAS TURBINE ENGINE FUEL SYSTEM | 2008 |
|
RU2379535C2 |
| METHOD OF GAS TURBINE ENGINE | 2011 |
|
RU2493392C2 |
| CONTROL METHOD OF GAS-TURBINE UNIT TECHNICAL CONDITION | 2009 |
|
RU2432562C2 |
| METHOD OF PROTECTION OF SHIPBOARD GAS TURBINE PLANT | 2011 |
|
RU2493393C2 |
| METHOD TO CONTROL FUEL FLOW RATE IN STARTING GAS TURBINE ENGINE | 2008 |
|
RU2386836C2 |
| CONTROL METHOD OF FUEL FLOW AT START OF GAS TURBINE UNIT | 2009 |
|
RU2422658C1 |
| CONTROL METHOD OF FUEL FLOW AT START OF GAS TURBINE UNIT | 2009 |
|
RU2427721C1 |
