The arrangement of the tuyere for aircraft a reaction of the type a lift-off vertical and / or a short lift-off

摘要

The invention relates to an aircraft, which comprises a fuselage 10, at least a tuyere rise in order to be able to be moved between a position directed towards the back and a position directed downwards, the arrangement being such that when the tuyere (or each tuyere) is directed downwards, the thrust thus produced is directed along a line located substantially in the same plane lateral that a first end available from the center of gravity of the aircraft (for example, the back). A balancing nozzle 22 is mounted so as to transfer of the gas to the - of the second end of the center of gravity (for example, the front) and willing in order to produce a component of the thrust of the balancing for compensating for the movement of the center of gravity of the aircraft between the first and second stiffener available. A tuyere may be rise of each side of the fuselage 10, thus allowing the figures of a component of the lace by a movement of the tuyeres differential.