Aircraft with a fuselage developed essentially as an aerostatic support body, drive unit with at least one propeller, in particular, for an aircraft and procedure for driving an aircraft with propeller drive.

摘要

B "AIRCRAFT WITH A FUSELAGE ESSENTIALLY DEVELOPED AS AEROSTATIC SUPPORT BODY, DRIVING UNIT WITH AT LEAST ONE PROPELLER, SPECIALLY, FOR AN AIRCRAFT AND PROCEDURE FOR CONDUCTING AN AIRCRAFT WITH HELDING." An aircraft having a fuselage developed essentially as an aerostatic support body and combined propulsion and support devices coupled to the fuselage, equipped with propellers and actuation units that are tilted in each support position, in which the plane of rotation of the respective propeller essentially horizontal and the drift axis of the coordinated drive, which admits the respective propeller axis, essentially vertical and a propulsion position, in which the rotation plane of the respective propeller is essentially vertical and the drift axis of the coordinated drive that allows the propeller shaft to be essentially horizontal. The plane of rotation of the propeller can rotate around the drift axis of the coordinated drive, which admits the respective propeller axis.