FIELD: aeronautical engineering.
SUBSTANCE: invention relates to aeronautical engineering, namely to vertical and short takeoff and landing aircraft. The VTOL convertiplane contains a folding rotor with a jet-compressor drive system. The drive system is provided with a separate turbocharger based on a gas turbine engine, which is installed in the upper part of the fuselage under the fairing in front of the wing center section, made according to the high-wing scheme. The turbocharger is equipped in front with a movable air intake flap, and at the rear with side exhaust pipes and a compressed air bleed pipe into the pipelines of the main rotor and the tail control ejector.
EFFECT: increased reliability and safety of use in conditions of folding and opening of the propeller in flight.
1 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SHORT TAKE-OFF AND LANDING TILTROTOR | 2022 |
|
RU2790460C1 |
| CONVERTIBLE PLANE | 2018 |
|
RU2682756C1 |
| VERTICAL TAKE-OFF AND LANDING AIRCRAFT WITH ROTOR WITH FOLDING RETRACTABLE BLADES | 2019 |
|
RU2727787C1 |
| MULTI-PURPOSE HIGH-SPEED HELICOPTER AIRCRAFT | 2017 |
|
RU2673317C1 |
| CONVERTIPLANE (VERSIONS) | 2010 |
|
RU2446078C2 |
| VERTICAL TAKE-OFF AND LANDING SEAPLANE WITH A MAIN ROTOR WITH FOLDING RETRACTABLE BLADES | 2021 |
|
RU2781817C1 |
| HEAVY-DUTY MULTI-PROPELLER CONVERTER PLATE | 2012 |
|
RU2492112C1 |
| CONVERTIPLANE WITH ROTORS JET DRIVE CONTROLLED BY ROTORS VIA WOBBLE PLATE AND CONTROL LEVERS WITH NO EXTRA CONTROL MEANS | 2013 |
|
RU2570241C2 |
| ROTOR-CRAFT | 2016 |
|
RU2662339C2 |
| VERTICAL TAKEOFF AND LANDING AIRCRAFT | 2015 |
|
RU2619976C2 |
