FIELD: transport.
SUBSTANCE: helicopter comprises wing (2) mounted on chassis (1) and equipped with rotors arranged on opposite sides. Wing features increased completed height and has appropriate load bearing set. Wing inside accommodates whatever hardware on helicopter complete set. Rotor axles (8) are inclined from helicopter axis of symmetry towards outward plane β=3°…6°. Projection of perpendicular to wing waterline onto helicopter plane of symmetry makes the angle γ=4°…10° to vertical.
EFFECT: higher speed and maneuverability.
2 cl, 5 dwg
Title | Year | Author | Number |
---|---|---|---|
SYNCHROCOPTER WITH FOLDING PROPELLERS | 2022 |
|
RU2783804C1 |
TRANSPORT AND COMBAT HELICOPTER (VARIANTS) | 2021 |
|
RU2768998C1 |
HEAVY HIGH-SPEED ROTARY-WING AIRCRAFT | 2016 |
|
RU2608122C1 |
UNMANNED CONVERTIPLANE ROCKET CARRIER AND METHOD FOR USE THEREOF | 2018 |
|
RU2699514C1 |
AIRCRAFT ROCKET COMPLEX WITH UNMANNED ATTACK HELICOPTER-AIRPLANE | 2017 |
|
RU2674742C1 |
VTOL AIRCRAFT | 2022 |
|
RU2788231C1 |
MULTIROTOR CONVERTIBLE PILOTLESS HELICOPTER | 2014 |
|
RU2550909C1 |
UNMANNED HIGH-SPEED HELICOPTER, DESANTIFIED FROM PLANE AIRCRAFT | 2016 |
|
RU2627975C2 |
MULTIFUNCTIONAL DOUBLE-SEAT WARPLANE OF ROUND-CLOCK ACTION, COMPLEX OF RADIO-ELECTRONIC EQUIPMENT USED IN THIS PLANE | 2008 |
|
RU2360836C1 |
UNMANNED VERTIPLANE WITH CHANNEL PROPELLERS | 2016 |
|
RU2629473C1 |
Authors
Dates
2009-11-20—Published
2008-01-25—Filed