The invention discloses a four-degree-of-freedom helicopter
tail rotor load measuring device in a wind tunnel, belongs to the technical field of helicopter
tail rotor
load measurement, and aims to solve the problem that an existing helicopter
tail rotor wind tunnel test lacks Z-direction accurate
displacement control. Comprising a
tail rotor assembly and a Z-direction adjusting mechanism, the Z-direction adjusting mechanism comprises a
barrel, a Z-direction bearing seat and a Z-direction motor mounting seat are arranged at the bottom of the
barrel, a Z-direction lead screw is in running fit with the Z-direction bearing seat, an output shaft of a Z-direction driving motor is coaxially connected with the lower end of the Z-direction lead screw through a Z-direction speed
reducer, a Z-direction nut is in threaded fit with the Z-direction lead screw, and a sliding sleeve is connected with the Z-direction nut. The upper end of the sliding sleeve is connected with the lower end of the
tail rotor supporting rod, the middle of the
tail rotor assembly is hinged to the upper end of the tail rotor supporting rod, the
yaw adjusting mechanism is arranged on the rear side of the tail rotor supporting rod, the output end of the
yaw adjusting mechanism is hinged to the rear portion of the tail rotor
assembly, and the tail rotor stand column is fixed to the output end of the XY-direction adjusting mechanism. The requirement for Z-direction movement of the helicopter tail rotor can be met.