| CPC B64C 17/06 (2013.01) | 25 Claims |
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1. A safety and stability device for an aircraft comprising:
an inner ring;
an outer ring that rotates relative to the inner ring;
a motor connected to the inner ring that drives rotation of the outer ring relative to the inner ring; and
a geared ring connected to the outer ring,
wherein the safety and stability device rotates in a substantially horizontal plane and at a rotational speed sufficient to provide gyroscopic stability for the aircraft.
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