FIELD: aircraft engineering.
SUBSTANCE: invention relates to an aircraft power plant. Power plant (10) comprises gas turbine engine (12), screw (14), rotating electrical machine (16). Power plant also comprises means (20) selective connection of rotating electrical machine (16) with screw (14) and/or gas turbine engine (12). Said means (20) are made with possibility of connecting only screw (14) with rotating electrical machine (16) during certain stage of power plant (10) operation, as well as with possibility of connection or not connection of rotating electrical machine (16) with gas generator and/or free turbine.
EFFECT: invention reduces fuel consumption, emission of exhaust gases and simplifies the steering process.
14 cl, 6 dwg
Title |
Year |
Author |
Number |
AIRCRAFT ENGINE AND ASSOCIATED METHOD FOR DRIVING FAN BY MEANS OF LOW PRESSURE SHAFT DURING TAXI OPERATIONS |
2016 |
|
RU2669759C2 |
POWER PLANT OF AIRCRAFT AND METHOD FOR OPERATION OF SUCH A PLANT |
2019 |
- Parmentier, Nicolas Claude
- Missout, Marc
|
RU2786896C2 |
HYBRID POWER PLANT OF MULTI-ENGINE AIRCRAFT |
2015 |
- Le Maux, David
- Mercier-Calvairac, Fabien
- Moulon, Frederic
|
RU2692513C2 |
METHOD AND AIRCRAFT WITH ROTATING LIFTING PLANE EQUIPPED WITH TWO MAIN GAS-TURBINE ENGINES AND AUXILIARY GAS-TURBINE ENGINE OF LESS POWER |
2013 |
|
RU2562084C2 |
METHOD FOR CONTROL OF ELECTRICITY GENERATION, USED FOR AIRCRAFT GAS TURBINE, AND APPARATUS FOR APPLYING SAID METHOD |
2011 |
|
RU2598476C2 |
PROPULSION UNIT OF AIRCRAFT, AND AIRCRAFT DRIVEN BY SUCH A PROPULSION UNIT BUILT IN REAR PART OF FUSELAGE OF AIRCRAFT |
2019 |
- Tantot, Nicolas, Jerome, Jean
- Gallet, Francois
|
RU2782719C2 |
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 |
METHOD AND DESIGN OF TURBINE MACHINE POWER COMBINING |
2011 |
- Bedrin Olive
- Markoni Patrik
- Puerto Alfons
|
RU2610872C2 |
GAS TURBINE ENGINE WITH REVERSIBLE ELECTRICAL MACHINE |
2009 |
- Bedrin Oliv'E
- Fo Monik
- Freall' Zhan-Ljuk
- Senzhe Zheral'
|
RU2499895C2 |
METHOD AND DEVICE FOR DETECTING GAS TURBINE ENGINE AIR INTAKE ICING |
2015 |
- Rossotto Rezhi
- Kami Emmanyuel
|
RU2608990C1 |