So, a Gyrocopter provides more options in case of emergency than a fixed wing and is less likely to experience a technical failure than a helicopter. A Gyroplane is a type of rotorcraft which uses an unpowered rotor in autorotation to develop lift, and an engine-powered propeller, similar to that of a fixed-wing aircraft, to provide thrust. While similar to a helicopter rotor in appearance, the rotor blades of a gyroplane are not powered. The rotor turns because of the passage of air through the rotor from below.
In the event of an engine failure, the gyroplane will descend, but the main rotor blades will continue to rotate and provide lift due to the continued airflow through them. Throughout flight, the gyroplane is therefore in a continuous state of autorotation and behaves similarly to a fixed wing aircraft, except that its wing rotates.
Most Gyrocopters are built around a metal chassis, to which everything else is mounted, like cars were until recent years. This provides a massive degree of safety for the crew in the event of any kind of accident, because the cabin is capable of withstanding loads that are many times the acceleration of gravity. In conclusion, the XENON cabin is the result of exploring leading edge technologies through hundreds of hours invested in analysis, testing and verification of the concept in practise, over 15 years of research and development.
Looking at the finished design you can perhaps now appreciate that virtually nothing was left to chance, every item is the result of many hours invested in the project to achieve the maximum safety, comfort and performance at the most efficient cost. Polish Tel.
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These cookies do not store any personal information. Skip to content WHY gyrocopters? Easy to Pilot. Complex to Pilot. Easy to maintain. Unlike a helicopter which has a powered rotor, the rotor of a gyroplane spins in flight due to the air loading on the rotor blades aerofoils as the aircraft moves forward. The free spinning rotor of a gyroplane does not require an anti-torque device, such as a tail rotor, as there is no torque load as would be associated with a powered rotor.
The most common gyroplane configurations are comprised of an airframe with landing gear, a single rotor which, in general, has either two or three blades, a propulsion engine and propeller in either pusher or tractor puller configuration, and an aircraft style tail assembly with a vertical fin and rudder , and a horizontal stabiliser and elevator.
The rudder and elevator flight controls work essentially the same as those of a conventional aircraft. A wing may be included in the design to enhance performance. A fundamental difference between helicopters and gyroplanes is that in powered flight, a gyroplane rotor system operates in autorotation. In other words, the rotor spins freely as a result of air flowing up through the blades, rather than using engine power to turn the blades and draw air down from above. Forces are created during autorotation that keep the rotor blades turning, as well as creating lift to keep the aircraft aloft.
Aerodynamically, the rotor system of a gyroplane in normal flight operates like a helicopter rotor during an engine-out forward autorotative descent.
Prior to takeoff, the gyroplane rotor must first achieve a rotor speed sufficient to create the necessary lift.
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