| 摘要 |
System for tilting a power unit (4) of an aircraft, said power unit (4) being located in the rear portion of the fuselage (1) of the aircraft, said system comprising a tilting unit (21) and a pivoting unit (6), with said tilting unit (21) permitting the tilting of the power unit (4) in a plane parallel to the vertical plane of the aircraft via the pivoting unit (6), giving rise to deflection of the exhaust gases from power unit (4), thus providing a vectorial thrust controllable independently for each power unit (4) of the aircraft, optimum for each phase of flight or manoeuvre of said aircraft, said component of vector thrust being deflected angularly in a plane parallel to the vertical plane of the aircraft and relative to the longitudinal axis of said aircraft.
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