MAI-205 is a single seater rotating-wing aircraft. It’s made from high-quality alloy steel, aluminium and titanium alloys, composite materials, textiles, etc.
The fuselage is made from aluminium tubes. The cockpit is fully enclosed with two doors with glazing made from organic glass. The nose fairing is made from glass-fibre plastic.
Tail unit is strut- and wire-braced, made from fabric covering aluminium tubes.
Landing gear — tricycle. The spring of main gear is made from titanium alloy. Main wheels (tire 300×125) are equiped with brakes. Brake system is hydraulic. The nose wheel (tire 300×125) is controlled by pedals.
Controls is mechanical, reversal. Autogyro is controlled through rotor hub control mechanism, rudder and elevator with controllable trimmer.
Rotor — two-bladed, made from fiberglass.
Jumping takeoff mechnism let autogyro realize jumping-off. Rotor comes untwisted at the ground, then pilot pushes the button on the control stick, the rotor-blade angle increases to 10 degrees, the autogyro jumps, then the rotor-blade angle decreases to 4 degrees and with the help of pusher airscrew autogyro turns into speed acceleration and climbing.
Instruments
- speed indicator US-250;
- compass KI-13;
- vertical speed indicator VR-10M;
- altimeter VM-3;
- bank indicator;
- rotor speed indicator;
- digital complex engine instrument FLYdat;
- digital chemicals counter.
Crop spraying equipment consists of:
- two 50-liter tanks for chemicals;
- filter;
- control set;
- rods and bracing wires;
- shut-off cock;
- branch pipe;
- electrical pump with a flowmeter and chemicals’ output counter;
- Russian atomizers or AU 7000 atomizers of the company MICRONAIR with shut-off valves and flow regulators.
Power plant.
Autogyro MAI-205 is equipped with Rotax—914ULS engine.
Rotax—914ULS engine — a four stroke, petrol, four-cylinder engine with turbo charger and electronic control of boost pressure, combined cooling and mixture formation in the carburettor. A two-blade propeller of fixed type is used for the engine.
Engine power of Rotax—914ULS is 100 hp at max. continuous perfomance and 115 hp at take-off perfomance. 30-liter fuel tank is integrated with 2 chemical tanks in a common removable unit.
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