A gas wing airflow directional aircraft comprises a machine body and a control room and is characterized in that the control room is arranged at the front part of the machine body, a lifting duct is arranged in the middle of the machine body, a propeller is arranged in the lifting duct, a gas separation bin plate with a herringbone longitudinal section is arranged below the propeller in the lifting duct, a transmission shaft of the propeller penetrates through a central hole of the air separation bin plate and is connected with a power transmission system in the control room, gas spraying windows are symmetrically formed in side walls of left and right sides of the lifting duct, the bottom end of the air separation bin plate is connected with the gas separation bin plate, wing-shaped airfoils are symmetrically arranged at the parts, outside the gas spraying windows, at the side walls of left and right sides of the lifting duct; the sections of the airfoils are outwards bulged arc surfaces; rear half parts, close to the machine body, of a propelling duct are symmetrically arranged at two sides of the machine body, and the rear part is connected with a propelling spraying tube, and a fan is arranged in the propelling duct. The gas wing airflow directional aircraft can form directional airflows, the airflows flow to the inside of the airfoils, and are then sprayed out from the bottom ends of the airfoils to form counter-acting force to the machine body so as to fast support the machine body.
Gas wing airflow directional aircraft
2015-11-11
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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