An aircraft rudder surface drive actuator performance test device
A test device and actuator technology, which is applied in the direction of aircraft component testing, etc., can solve the problems of difficulty in measuring the output force of the airborne actuator, inconvenient installation of the loading system, and scattered stiffness simulation, so as to save development costs, design flexibility, and The effect of reducing force
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[0021] The present invention will be described in further detail below in conjunction with the accompanying drawings of the description, please refer to figure 1 , figure 2 , image 3 .
[0022] Such as figure 1 As shown: the device includes a support, a rudder surface driving actuator 5, a rudder surface simulation part 6 and a loading actuator 7; the rudder surface simulation part 6 includes rocker arms 6-1, 6-3, The mass plate 6-2 and the rotating shaft 6-4, the rocker arms 6-1, 6-3 are fixedly connected with the rotating shaft 6-4, the mass plate 6-2 is symmetrically fixed on both ends of the rotating shaft 6-4; the rudder surface drives the actuator 5 One end is fixed by the support, and the other end is connected to the rudder surface simulation part 6 by the rocker arm 6-1. One end of the loading actuator 7 is fixed by the support, and the other end is connected to the rudder surface simulation part 6 by the rocker arm 6-3.
[0023] The performance test device of t...
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