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Simple and Strong Aircraft


The K-Max owes its performance to the Flettner double-rotor principle. It allows heavy loads to be transported with relatively low engine power. Thanks to the counter-rotating main rotors, the K-Max does not need a tail rotor; this saves weight and drive power.


The counter-meshing two-blade rotors are fixedly synchronized at 90 degrees via the main gear. The rotor blades are controlled using the Flettner flap on the rear edge of each blade. The control forces remain low, and there is no need for hydraulic assistance as on traditional helicopters.


The aluminum half-shell fuselage is just wide enough to accommodate the pilot as well as the engine with transmission


54 Sept/Oct 2024


and fuel tank. The narrow shape ensures strong stability of the cell, especially for a better absorption of forces. Thanks to the simplicity of the construction, the empty mass remains low. Additionally, in the narrow fuselage, the pilot has a direct view of the external load from both sides of the cockpit. An armrest and a support on the fuselage ensure a comfortable seating position for the pilot during flights with loads, and this increases precision.


The first flight of the K-Max took place in 1991, and no major modifications have been made to the machine since production began; its construction is still solid today. However, the safety of the helicopter could be improved by strengthening the freewheel clutch, which sometimes caused problems in the early years. For the future, the manufacturer has promised further improvement of the rotor blades.


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