CONVERTIBLE A ROTOR BLOQUE A L'AVANT DU FUSELAGE EN VOL HORIZONTAL

摘要

The aircraft has a rotor whose two blades are placed in front of a fuselage and produce bearing pressure necessary for a girodyne mode during rotation of the rotor. The blades produce a part of the pressure when the blades are stopped and blocked in an airplane mode. A common drive system is utilized in the girodyne and airplane modes. The drive system comprises even number of engines placed on the blades along both sides of a rotation axis. The drive system is placed in a position on the blades such that output of the drive system is maximized at same time in the girodyne and airplane modes.