THREE-ENGINED ROTODYNE Russian patent published in 2012 - IPC B64C27/22 

Abstract RU 2460671 C1

FIELD: transport.

SUBSTANCE: three-engined rotodyne comprises rotor/rotors and tractor or pusher propeller/propellers or compressor/compressors of turbojet second circuit. second circuit. Rotodyne comprises three engines one which serves to transmit power to only rotor, while other two engines transfer power to rotor and tractor or pusher propeller, or compressor. Rotodyne may have transverse, coaxial or lengthwise configurations. Engines may be arranged either in line across rotodyne, or two engines may be located on fuselage sides and one inside or on fuselage, or one engine may be arranged nearby front propeller and two nearby rear propeller.

EFFECT: higher reliability.

4 cl, 7 dwg

Similar patents RU2460671C1

Title Year Author Number
MULTIROTOR HELICOPTER (VERSIONS) 2007
  • Staroverov Nikolaj Evgen'Evich
RU2351505C2
MULTIPURPOSE MULTI-TILTROTOR HELICOPTER-AIRCRAFT 2010
  • Durov Dmitrij Sergeevich
RU2448869C1
UNMANNED ROTORCRAFT WITH CROSS-SECTION PROPELLERS 2016
  • Durov Dmitrij Sergeevich
RU2627963C1
RESCUE HELICOPTER (VERSIONS) 2006
  • Staroverov Nikolaj Evgen'Evich
RU2335432C2
HIGH-SPEED HELICOPTER WITH CROSSED SCREWS 2016
  • Durov Dmitrij Sergeevich
RU2636826C1
MULTI-PURPOSE TWO-FUSELAGE HELICOPTER AIRCRAFT 2017
  • Durov Dmitrij Sergeevich
RU2650258C1
MULTIPURPOSE HELICOPTER AIRPLANE WITH REMOTE CONTROL 2008
  • Durov Dmitrij Sergeevich
RU2370414C1
MULTIROTOR HIGH-SPEED HELICOPTER-AIRCRAFT 2017
  • Durov Dmitrij Sergeevich
RU2658736C1
SHORT HELICOPTER (VERSIONS) 2006
  • Staroverov Nikolaj Evgen'Evich
RU2356795C2
HIGH-SPEED TURBOFAN COMBINED HELICOPTER 2016
  • Durov Dmitrij Sergeevich
RU2629475C1

RU 2 460 671 C1

Authors

Staroverov Nikolaj Evgen'Evich

Dates

2012-09-10Published

2011-06-22Filed