Abrasion test device for aircraft control connecting rod

The invention discloses an aircraft control connecting rod wear test device, which comprises a basic frame, a swing motion mechanism, a rotating shaft mechanism and an axial loading mechanism, and is characterized in that the axial loading mechanism is used for applying an axial load to a push-pull rod, and the rotating shaft mechanism comprises a rotating shaft sleeved with a rod end joint bearing; the swing motion mechanism is connected with the rotating shaft, and drives the rotating shaft to rotate relative to the rod end knuckle bearing through reciprocating swing. The aircraft control connecting rod wear test device can simulate the wear environment of a typical control connecting rod structure of a general aviation aircraft and test, can provide effective data support for operation and maintenance of the general aviation aircraft, and has the advantages of low cost, high reliability, high adaptability, convenience in test implementation, reachability, safety, high efficiency and the like. 本发明公开了一种飞机操纵连