Improved aerodynamic rotor shape suitable for small and medium-sized unmanned tilt rotor aircrafts
A tilt-rotor, aerodynamic shape technology, applied in unmanned aerial vehicles, aircraft, rotorcraft, etc., can solve the problems of late start of tilt-rotor, complex design requirements of tilt-rotor blades, etc. The effect of high cruising efficiency, reduced form resistance and low actual power
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[0025] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
[0026] The purpose of the present invention is to provide an improved rotor aerodynamic profile suitable for small and medium-sized unmanned tilt rotor aircraft, which improves the aerodynamic performance of the rotor aerodynamic profile in hovering and flying states.
[0027] In order to make the above objects, features and advantages of the present invention more comprehensible, the present invention will be further described in detail below in conjunction wi...
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