RES Monocopter

RES - Helicopter 1
#towhomitmayconcern : The patent lnkd.in/gFesNkZY reveals a comprehensive universality for fluid machines serving different purposes. lnkd.in/d2P9mhhQ The scope of the invention relates to embodiment of hull integrated propulsion systems, #resship, to rotary wing aircraft, #resaircraft, to wind turbines, #reswindpower as well as to water turbines #reshydropower. Patent granted for #resheli1 the first and only helicopter #asktheinventor with a rotor integrated propeller. What is claimed is : Device for a rotary-wing vehicle or for a rotary-wing turbine, which device has at least one rotor module with rotary-wing kinematics for at least two kinematic rotor blades connected to a motor generator and rotating on an orbit about an axis of rotation, which rotor blades are subdivided into a plurality of longitudinal sections for receiving in each case at least one actuator integrated in a longitudinal or transverse spar of the rotor blade and have a variable asymmetrical airfoil profile which is adjustable in a revolution of the rotor blade at a diameter of the revolution path freely orientable within an adjustment range with two turning points lying opposite each other on a diameter of the revolution path in at least one longitudinal section of the rotor blade with a length in such a manner that the suction side (-) and the pressure side (+) of the asymmetrical blade profile changes from the outside to the inside of the orbit by means of the rotary blade kinematics at the turning points or vice versa and the variable blade profile of the rotor blade in a transition position at the turning points temporarily has a symmetrical blade profile oriented with its profile chord tangential to the orbital path, the device being designed, in the case of the design on the rotary-wing vehicle, in such a way that the diameter with the turning points on the rotor module can be aligned in the at least one longitudinal section of the rotor blades with the length transverse to the direction of travel so that the suction side (-) of the asymmetrical airfoil is oriented in the direction of travel in both halves of the orbital path and a thrust force acting in the direction of travel results from the lift force generated on the asymmetrical airfoil, and wherein, in the case of the design on the rotary blade turbine, the device is designed in such a way that the diameter with the turning points in all longitudinal sections of the rotor blade can be aligned orthogonally to the flow, so that the suction side of the asymmetrical airfoil can be oriented to the lee side in both halves of the orbital path and a tangential drive force for the rotary-wing turbine results from the lift force generated by the asymmetrical airfoil. #resmonocopter #aviation #aerospace #research #fluiddynamics #electricflight #aerodynamics #advancedairmobility #futureofmobility #theländ #notforeverybody www.res-instit...
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