FIELD: testing equipment.
SUBSTANCE: stand for modelling the impact of aerodynamic load on opening elements of aircrafts comprises a base on which an opening mechanism with opening element is fixedly mounted, as well as a loading mechanism connected kinematically with the opening element. The stand is provided with pulleys and a beam which is parallel to the axis of rotation of the opening element and rigidly mounted on the pulleys, which are fixed on the base with the ability of rotation and interaction with a loading mechanism. The axes of rotation of the pulleys coincide with the axis of rotation of the opening element.
EFFECT: improved accuracy of modelling the impact of aerodynamic load.
5 cl, 3 dwg
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