LOAD SIMULATOR FOR FLIGHT CONTROL ACTUATION SYSTEM HAVING STIFFNESS IMPLEMENTAL DEVICE OF AIRFRAME MOUNTING STRUCTURE

摘要

A load simulator for flight control actuation system having stiffness implemental device of airframe mounting structure is provided to test the dynamic load characteristic test in the airframe mounting condition. The load simulator for flight control actuation system comprises the moment of inertia(2) copying the rotating inertia load, the moment arm(4) assembled in the shafting plane column shape, the load servo driver(6) copying the aviation load generated in flying, the location servo driver(5) performing the rotational fluctuation control of exercise of the operation object, the airframe structure supporting part rigidity realization equipment assembling(9) supporting the location servo driver, the simulator frame(10) supporting the moment arm, the driver neutrality road and the row information commercial gap phase.