A rotorcraft (or rotary wing aircraft)
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 |
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The fcfawira is the meosurement data under standard atmoscharicptotsult mnndsens wih aximum load of 563kg oft he aircraft |