FIELD: aeronautical engineering. SUBSTANCE: device has tail boom 1 and end boom connected with boom 1. Steering rotor 3 is mounted on end boom 2. Device has transmission system 4 for drive of steering rotor 3. Detachable unit 5 consisting of parts of fuselage interconnected by screws includes powder charge unit. EFFECT: high safety of flight due to sufficient amount of time for estimation of situation in taking decision by pilot in case of autorotation regime. 7 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| APPARATUS FOR COMPENSATING THE REACTIVE TORQUE OF THE MAIN ROTOR OF A HELICOPTER | 2021 |
|
RU2788013C1 |
| HELICOPTER AND METHOD OF CONTROL OF SINGLE-ROTOR HELICOPTER | 2002 |
|
RU2238221C2 |
| HELICOPTER MAIN ROTOR TORQUE COMPENSATION DEVICE | 2021 |
|
RU2796703C2 |
| SYSTEM FOR COMPENSATION OF REACTION TORQUE OF MAIN ROTOR OF SINGLE-ROTOR HELICOPTER | 2003 |
|
RU2245821C1 |
| SYSTEM FOR WARNING THE PILOT ABOUT THE OCCURRENCE OF AN UNINTENTIONAL TURN TO THE LEFT OF A SINGLE-ROTOR HELICOPTER | 2022 |
|
RU2782807C1 |
| METHOD FOR PREVENTING SPONTANEOUS ROTATION OF A HELICOPTER | 2022 |
|
RU2782038C1 |
| HIGH SPEED AND MANEUVERABILITY ROTORCRAFT | 2012 |
|
RU2480379C1 |
| HIGH-SPEED TURBOELECTRIC HELICOPTER | 2013 |
|
RU2521090C1 |
| FAST-SPEED COMBINED HELICOPTER | 2016 |
|
RU2610326C1 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH ROTOR WITH FOLDING RETRACTABLE BLADES | 2019 |
|
RU2727787C1 |
