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Airplane e.g. civil transport aircraft, has wing mounted movably with respect to fuselage along longitudinal direction parallel to axis of fuselage between front extreme position and rear extreme position of reference point of wing
Airplane e.g. civil transport aircraft, has wing mounted movably with respect to fuselage along longitudinal direction parallel to axis of fuselage between front extreme position and rear extreme position of reference point of wing
The airplane (1) has a wing (3) integrated with a fuselage (2) on a level of a central box. An assembly (4) of tail empennages is integrated with the fuselage. The wing is mounted movably with respect to the fuselage along a longitudinal direction (X) parallel to an axis of the fuselage between a front extreme position and a rear extreme position of a reference point of the wing. A guiding unit is integrated to the central box and supported on parallel beams allowing movement of the wing.
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