A helicopter has a main rotor with propeller blades which is driven by a rotor shaft and which is hinge-mounted to this rotor shaft. The angle between the surface of rotation of the main rotor and the rotor shaft may vary. A swinging manner on an oscillatory shaft is essentially transverse to the rotor shaft of the main rotor and is directed transversally to the longitudinal axis of the vanes. The main rotor and the auxiliary rotor are connected to each other by a mechanical link. The swinging motions of the auxiliary rotor controls the angle of incidence (A) of at least one of the propeller blades of the main rotor. There are wings from the body and a stabilizer at the tail.
RELATED APPLICATION
This application is a Continuation of U.S. patent application Ser. No. 11/754,752, filed Jun. 14, 2007, which is a Divisional of U.S. patent application Ser. No. 11/465,781 filed on Aug. 18, 2006, which is a Continuation-in-Part of U.S. patent application Ser. No. 11/462,177, filed on Aug. 3, 2006 and entitled HELICOPTER, which claims priority to Belgian Patent Application No. 2006/0043 entitled AUTOSTABIELE HELICOPTER by Alexander VAN DE ROSTYNE, which was filed on Jan. 19, 2006. The contents of these applications are incorporated by reference herein.
