CPC B64C 21/02 (2013.01) [B64C 1/0009 (2013.01); B64F 5/00 (2013.01)] | 16 Claims |
1. An aircraft comprising:
a fuselage including an inner structure configured to house operational components and an empty cavity separate from the inner structure, the empty cavity extending from a front of the fuselage to a rear of the fuselage;
one or more wings extending from the fuselage;
an outer skin defining the empty cavity of the fuselage; and
one or more apertures comprising at least a first aperture and a second aperture in the outer skin of the fuselage;
wherein the one or more apertures are configured to enable air to pass through the empty cavity of the fuselage by passing through the one or more apertures when the aircraft is flying; and
wherein the first aperture is positioned in an upper central portion of the aircraft and the second aperture is positioned on a side of the aircraft.
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