Patent ID: 6969026

Claim:
An aircraft comprising: a main body; a first pair of sub bodies positioned respectively in left and right sides of the main body and substantially in parallel with the main body; plural wings which are fixed to the main body at central portions of the wings and are also fixed to the sub bodies at those portions of the wings that are close to both left and right ends of the wings; another pair of sub bodies positioned in parallel with the main body, respectively in both left and right sides of the main body and the first pair of sub bodies, and engines respectively mounted on outer surfaces of the sub bodies, wherein the sub bodies are thinner than the main body, one or the wings, which is positioned closest to the fore end of the aircraft among the wings and serves as a first canard, has a shorter wing span than the other wings, and fuel is contained in the sub bodies and is supplied to the engines mounted on the sub bodies.