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A rotorcraft (or rotary wing aircraft)

rotorcraft

A rotorcraft (or rotary wing aircraft)

Mainly used in short-distance transport, recreational flying, air rescue, aerial security patrol, oil and electricity patrol, plant protection of agriculture and forestry, tourism development. With the development of society, rotorcraft will have more extensive application in different fields.

The J-RO series Gyrocraft offers outstanding maneuverability and flight experience. Pilots can directly feel the quick response and sensitivity of the control stick in controlling the aircraft. The powerful engine allows for steep climbs and high-G turns, stimulating every nerve in the body. With an open cockpit, one can directly connect with the sky and clouds, experiencing the sensation of soaring like an eagle!

    advantage

    A rotorcraft (or rotary wing aircraft) is a heavier-than-air aircraft that uses lift generated by wings, called rotor blades, that revolve around a mast. Several rotor blades mounted to a single mast are referred to as a rotor. The International Civil Aviation Organization (ICAO) defines a rotorcraft as supported in flight by the reactions of the air on one or more rotors

    Since the rotor of the rotorcraft is unpowered, it does not have large vibrations and noises caused by the power-driven rotor system. This vibration and noise will not shorten or increase the service life of the rotor, body, etc. Occupant fatigue. The impact caused by the rotorcraft's power-driven propeller is obviously much smaller.

    The gyrocopter can automatically adjust so that the fuselage has good pitch stability, roll stability and speed stability. The rotating propeller disk is like a large inertial wheel, and the rotor has no periodic pitch changes. In addition, the rotor installation angle is larger than that of the helicopter, which has better gyroscopic effect, higher stability and strong wind resistance.

    specifications

    Number of seats

    2

    leag.th (including rotors)

    8.6m

    Height (including rotors)

    2.72m

    Length of fuselage

    4.95m

    Maximum width of fuselageTake off roll

    1.9m

    Take off roll

    80-120m

    Landing distance

    0-30m

    Maximum crosswind speed

    10.5m/s

    Maximurn Headwind Spced

    20m/s

    Flight height

    3200m

    Maximum spoed never excued

    180km/h

    Duration of ftight

    3.2hours

    Temperature range

    -20℃ to+35/40℃

    Engine type

    ROTAX 914UL

    Rated engine power

    115cv/hp

    Empty weght

    309kg

    Maximum take off weight

    560kg

    Speed for maximu m endu rance

    100km/h

    Cruise speed

    130km/h

    Fuel capacity

    70L

    Fuel type

    RON95PLeadjethanal-free motor gasoline ot RON95# or above

    The fcfawira is the meosurement data under standard atmoscharicptotsult mnndsens wih  aximum load of 563kg oft he aircraft