FIELD: transport.
SUBSTANCE: aircraft with longitudinal and circumferential curvature includes set of devices (80) of force application to the fuselage rim. It includes central rigid shaft (20) located in longitudinal direction and on the centre of rim (10) of fuselage and having the possibility of fixed joint with rim (10) of fuselage. Set of force application devices is installed between fuselage rim and support devices (70, 90) rigidly attached to central rigid shaft (20).
EFFECT: development of testing device of the fuselage construction with longitudinal and circumferential curvature.
11 cl, 12 dwg
