This invention provides a composite static and
fatigue testing apparatus for aero-engine shaft components, comprising a load-bearing frame, a torque loading device, a shaft clamping device, a loading
actuator, a torque limiting device, an
axial force and
bending moment loading device, and a test shaft. The shaft clamping device includes a lower connecting shaft, a deep groove
ball bearing, and a lower bearing section, used to connect and fix the test shaft and connect the torque loading device and the
axial force and
bending moment loading device, and to transfer the load to the load-bearing frame. The torque limiting device and the
axial force and
bending moment loading device are used to load the required axial force and rotational bending moment onto the test shaft, and to decouple the loading of axial force and rotational bending moment. The shaft clamping device is connected to the torque loading device. The shaft clamping device is equipped with a lower connecting shaft, a deep groove
ball bearing, and a lower bearing section, so that the axial force and rotational bending moment can be loaded using the same loading device. It is suitable for testing aero-engine shaft components with different load requirements.