FIELD: physics.
SUBSTANCE: device has apparatus (30, 40) for applying force to the crown (10) of the fuselage with a longitudinal and circular curvature. The device has support apparatus (50) on which the crown (10) of the fuselage can be fitted and apparatus (30, 40) for applying force. The apparatus (30, 40) for applying force are placed between the said support apparatus (50) and the force transmission apparatus (70) which are immovably connected to the crown (10) of the fuselage, and are configured to apply twisting and tensile/compression forces, which are tangential at the point of their application to the crown (10) of the fuselage.
EFFECT: testing the fuselage structure with double curvature with reconstruction of real situations acting on the fuselage structure of an aeroplane.
13 cl, 16 dwg
