FIELD: transport.
SUBSTANCE: invention relates to aircraft, specifically to bearing assembly for installation of a pair of mutually spaced parallel actuators between a wing and control surface of aircraft so that the actuators collectively control the deployment of the mentioned surface out of wing. The bearing assembly contains immovable element to be attached to aircraft and movable element made capable to be attached to actuators. Immovable and movable elements are connected by means of partially spheric bearing and are made so that partially spheric bearing is located in the space between actuators.
EFFECT: smaller dimensions of actuating system for wing control surfaces control.
15 cl, 4 dwg
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