FIELD: aircraft engineering.
SUBSTANCE: helicopter incorporates rotor and tail rotor, airframe comprising the crew cab with controls, step-down gearing with two opposite-rotation shafts, swashplate, chassis, tail boom furnished with horizontal stabiliser, keel, rudder and elevator. The tail rotor is arranged under the airframe in special shell. Load system and water jet are also arranged under the airframe.
EFFECT: reduced helicopter weight, operation under whatever flying conditions, better performances.
2 dwg
Title | Year | Author | Number |
---|---|---|---|
HELICOPTER | 2010 |
|
RU2452659C1 |
FIRE CRANE HELICOPTER | 2022 |
|
RU2797539C1 |
UNMANNED HIGH-SPEED HELICOPTER, DESANTIFIED FROM PLANE AIRCRAFT | 2016 |
|
RU2627975C2 |
HIGH SPEED AND MANEUVERABILITY ROTORCRAFT | 2012 |
|
RU2480379C1 |
SINGLE-ROTOR HIGH-SPEED HELICOPTER | 2022 |
|
RU2770945C1 |
ROTOR-CRAFT | 2016 |
|
RU2662339C2 |
CONVERTIPLANE WITH ROTORS JET DRIVE CONTROLLED BY ROTORS VIA WOBBLE PLATE AND CONTROL LEVERS WITH NO EXTRA CONTROL MEANS | 2013 |
|
RU2570241C2 |
VERTICAL TAKE-OFF AND LANDING SEAPLANE WITH A MAIN ROTOR WITH FOLDING RETRACTABLE BLADES | 2021 |
|
RU2781817C1 |
HIGH-SPEED TURBOELECTRIC HELICOPTER | 2013 |
|
RU2521090C1 |
FIREFIGHTING AIRCRAFT | 2010 |
|
RU2483981C2 |
Authors
Dates
2008-11-20—Published
2006-10-02—Filed