CPC B64C 39/04 (2013.01) [B64C 39/02 (2013.01)] | 2 Claims |
1. An aircraft having a main fuselage, and two a pairs of left and right auxiliary fuselages, that the two pairs of left and right auxiliary fuselages are connected by a front wing, a main wing, and a horizontal stabilizer wherein;
a chord of the front wing, a chord of the main wing, and a chord of the horizontal stabilizer are all almost constant over the entire length;
a narrow portion of the chord of the main wing is provided at a connection portion between the main fuselage and the main wing;
a cross section of each of the two pairs of left and right auxiliary fuselages is a perfect circular; and
booms made of rigid pipes for aerial refueling along the outer wall surface of the two pairs of left and right auxiliary fuselages.
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