Patent ID: 8464977
Filing Date: 2013-06-18
Classification: B60V,B64B,B64C

Abstract:
1. A positive-pressure flying aircraft comprising: a main body having a front end; a right body disposed at one side of the main body and having a front end; a left body disposed at the other side of the main body and having a front end, the front ends of the right and left bodies being behind the front end of the main body; a wing supported by the main body, the right body and the left body and having a front end that is behind the front ends of the right and left bodies, an air path being defined longitudinally of the aircraft by a bottom surface of the wing and inner side surfaces of the right and left bodies; a horizontal stabilizer; a thrusting device in a gap; a vertical fin in the middle of the horizontal stabilizer; a rudder at the rear end of the vertical fin; and an elevator at the rear end of the horizontal stabilizer, wherein the wing has an upper surface which is flat and a lower surface with a positive camber, and the horizontal stabilizer has an upper surface with a positive camber and a lower surface which is flat, the wing gradually getting thinner rearward from a maximum thickness portion, the gap being formed between the wing and the horizontal stabilizer.