| CPC B64C 39/12 (2013.01) [B64C 29/0025 (2013.01); B64C 39/08 (2013.01)] | 8 Claims |

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1. An aircraft comprising:
a fuselage having a front end and a rear end, said fuselage having a starboard side and having a port side opposite said starboard side;
a first wing, said first wing positioned above a second wing;
said first wing having a first wingtip positioned on said starboard side of said fuselage and having a second wingtip positioned on said port side of said fuselage;
said second wing having a first wingtip on said starboard side of said fuselage, and having a second wingtip positioned on said port side of said fuselage;
a first rotor assembly positioned in between a distal end of said first wingtip of said first wing and a distal end of said first wingtip of said second wing;
a second rotor assembly positioned in between a distal end of said second wingtip of said first wing and a distal end of said second wingtip of said second wing;
said first rotor assembly having a first propeller including a plurality of blades projecting radially therearound from respective engagements thereto, said first propeller being engaged with a first motor generator, said plurality of blades extending from said first propeller rotating in a horizontal plane in the same direction, said horizontal plane extending into a gap between said first wing and said second wing; and
said second rotor assembly having a second propeller including a plurality of blades projecting radially therearound from respective engagements thereto, said second propeller being engaged with a second motor generator, said plurality of blades of said second propeller rotating in said horizontal plane in the same direction.
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