FIELD: motors and pumps.
SUBSTANCE: specific fuel consumption optimization method of helicopter equipped with two gas turbine engines (1, 2), each of which contains equipped with the combustion chamber (CC) gas generator (11, 21), at that, each of these gas turbine engines (1, 2) is configured to operate independently in the constant flight mode, and in this case the other gas turbine engine (2, 1) is in the so-called super-low gas mode with zero power and with switched on combustion chamber (CC), wherein this super-low gas mode is maintained by mechanically driving the gas generator shaft (AE) into rotation in this mode so, that to reduce this gas generator operating temperature and fuel consumption.
EFFECT: proposed is the helicopter specific fuel consumption optimization method.
4 cl, 1 dwg
| Title |
Year |
Author |
Number |
| METHOD OF OPTIMISING SPECIFIC CONSUMPTION OF TWIN-ENGINE HELICOPTER AND A TWIN-ENGINE STRUCTURE WITH CONTROL SYSTEM TO THIS END |
2011 |
- Markoni, Patrik
- Tire, Romen
|
RU2593317C2 |
| GAS TURBINE ENGINE, TWIN-ENGINE HELICOPTER EQUIPPED WITH SUCH GAS-TURBINE ENGINE, AND OPTIMIZATION METHOD OF SUPER-LOW GAS MODE WITH ZERO POWER OF SUCH TWO-ENGINE HELICOPTER |
2015 |
- Thiriet, Romain
- Bedrine, Olivier
- Marconi, Patrick
|
RU2687469C2 |
| TURBOSHAFT ENGINE COMPRISING CONTROLLED MECHANICAL COUPLING DEVICE, HELICOPTER EQUIPPED WITH SUCH TURBOSHAFT ENGINE, AND METHOD FOR OPTIMISING ZERO-POWER SUPER-IDLE SPEED OF SUCH HELICOPTER |
2015 |
- Marconi Patrick
- Thiriet Romain
- Serghine Camel
|
RU2674861C2 |
| HELICOPTER MULTIMOTOR POWER SYSTEM AND CORRESPONDING HELICOPTER |
2015 |
- Mercier-Calvairac Fabien
- Humbert Sophie
- Beddok Stephane
|
RU2702377C2 |
| MULTI-ENGINE HELICOPTER POWER SYSTEM ARCHITECTURE AND CORRESPONDING HELICOPTER |
2015 |
- Merse-Kalverak Faben
- Beddok Stefan
- Shevale Stefan
- Yumber Sofi
|
RU2690608C2 |
| METHOD FOR AUTOMATIC CONTROL OF OPERATING MODE OF HELICOPTER GAS TURBINE ENGINE, CORRESPONDING CONTROL DEVICE AND HELICOPTER EQUIPPED WITH SUCH DEVICE |
2014 |
- Sev Karolin
- Pumared Vensan
- Tire Romen
|
RU2693957C1 |
| METHOD OF AMPLIFYING GAS TURBINE ENGINE IN STANDBY MODE OF MULTI-ENGINE HELICOPTER AND STRUCTURE OF HELICOPTER POWER PLANT COMPRISING AT LEAST ONE GAS TURBINE ENGINE WHICH CAN BE IN STANDBY MODE |
2015 |
- Bedrin Olive
- Deskyub Olive Per
|
RU2689266C2 |
| PNEUMATIC DEVICE FOR FAST REACTIVATION OF GAS TURBINE ENGINE, POWER PLANT STRUCTURE OF MULTI-ENGINE HELICOPTER EQUIPPED WITH SUCH DEVICE AND CORRESPONDING HELICOPTER |
2015 |
- Thiriet Romain
- Moulon Frederic
- Serghine Camel
|
RU2703862C2 |
| HYDRAULIC DEVICE FOR EMERGENCY STARTING A TURBINE ENGINE, PROPULSION SYSTEM OF A MULTI-ENGINE HELICOPTER PROVIDED WITH SUCH DEVICE, AND CORRESPONDING HELICOPTER |
2015 |
- Thiriet, Romain
- Moine, Bertrand
- Serghine, Camel
- Porel, Francois
|
RU2672219C2 |
| METHOD AND AIRCRAFT WITH ROTATING LIFTING PLANE EQUIPPED WITH TWO MAIN GAS-TURBINE ENGINES AND AUXILIARY GAS-TURBINE ENGINE OF LESS POWER |
2013 |
|
RU2562084C2 |
