摘要 |
The present invention herein is a disc shaped wing comprised two disc segments, an inner disc assembly and an outer disc assembly, that counter-rotate to enable vertical take off and landing. The inner disc assembly has a plurality of flap blades that open to provide lift during take off and landing and close to provide a substantially contiguous surface during horizontal flight. The outer disc assembly has a plurality of lower blades that contain retractable blades. During take off and landing the retractable blades extend to provide added lift and stability. The wing shape and counter-rotation also imparts greater stability and lift for horizontal flight.
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