FIELD: aviation.
SUBSTANCE: invention relates to the field of aviation, in particular to the methods for converting a wing in the rotor. Method for converting disk wing in the rotor and back, is that the blade is put forward from the disc of the wing by its inertial force, rotating in the plane of the disc relatively the solid gland, which connects the blade root with the disc perimeter in the gap formed between the disk parts. Parts of the disc are pushed by the torsion links, loaded in their middle glands by inertial mass forces located in the centripetal acceleration of the disc. The blades are hidden in the gap by the toothed belt reinforced with one end of the blade, and with the other which engages with the drum located on the shaft in the center of the disc. Drum braking creates tension of the toothed belt and hiding of the blade rotating it in the crater of the disc on the carriages along the rails, determining the angle of attack and stroke of the blade in the operating position, and direction of its movement in the plane of rotation at the entrance in the disc gap.
EFFECT: invention provides a release and hiding of the blades of complex aerodynamic shape.
4 dwg
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Authors
Dates
2017-02-06—Published
2015-07-31—Filed