| 摘要 |
<p>The aircraft has a pivoting motor for swinging a moving part carrying a rear rotor (10) from a fixed position (POS1) to another position in a reversible manner so that the aircraft passes from an operating mode to another operating mode during which propulsion of the aircraft is assured by the rear rotor. An inclination unit inclines a mast in an anteroposterior longitudinal plane toward a rear end (4'') of the aircraft in a reversible manner so that the aircraft passes from the latter mode toward a third operating mode during which propulsion of the aircraft is assured only by the rear rotor. An independent claim is also included for a method for piloting an aircraft.</p> |
