Aircraft structure

An aircraft structure comprising:

• a fuselage;
• first and second forward wings mounted to and/or extending from opposing sides of the fuselage;
• a continuous rear wing span defining first and second rear wings and a central static connecting portion;
• a first wing connecting member extending between the first forward wing and the first rear wing;
• a second wing connecting member extending between the second forward wing and the second rear wing;
• and
• first and second electric motors each having rotors, are mounted to each wing, each rotor is pivotal between a first configuration for vertical flight, and a second configuration for forward flight,
• wherein the rear wing span is supported by a centrally located V tail joint defined by first and second angularly inclined arms, and
• wherein the first and second angularly inclined arms are joined at a proximal lower end, and wherein the proximal lower end is mounted between a rear bulkhead of the fuselage and a tail cone such that the proximal lower end is internally housed in an internal cavity formed by the rear bulkhead and the tail cone.