CPC B64C 29/0033 (2013.01) [B64C 39/066 (2013.01)] | 12 Claims |
1. An air mobility device comprising:
a main body;
compression motors provided in the main body so as to form compressed air;
wings installed on the main body so as to be rotatable and configured to have respective open spaces formed therein such that external air passes through the open spaces and the compressed air formed by the compression motors flows into the wings and is discharged to the open spaces; and
blowers configured to generate air flow so as to generate propulsion and installed at positions of the open spaces of the wings, to which the compressed air is discharged, such that the compressed air flows into the blowers so as to increase the propulsion,
wherein each of the wings comprises a first wing panel and a second wing panel installed on the main body,
wherein the first wing panel and the second wing panel form an inner space so as to circulate the compressed air transmitted by at least one of the compression motors, and the first wing panel and the second wing panel are spaced apart from each other so as to form the open space therebetween, and
wherein first discharge holes configured to discharge the compressed air are formed in the first wing panel, second discharge holes configured to discharge the compressed air are formed in the second wing panel, and the first discharge holes and the second discharge holes are disposed to face each other.
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