Calibration device of aero-engine axial force measurement structure

The invention belongs to the field of axial force measurement of an aero-engine thrust bearing, and particularly relates to a calibration device of an aero-engine axial force measurement structure, which comprises a support frame/a support platform/a pressure device/a pressure head/a pressure plate and a bearing platform, according to the invention, an axial force measuring structure assembly can be directly connected through the flange edge, the device also has a function of adjusting the position and posture of a test piece, and the operation steps of testers are simplified. 本发明属于航空发动机推力轴承的轴向力测量领域，具体设涉及一种航空发动机轴向力测量结构的标定装置，包括支撑框架/支撑平台/加压装置/压头/压板以及承件平台；本发明能直接通过法兰边来连接轴向力测量结构组件，同时还具有试验件位置、姿态的调节功能，简化试验人员的操作步骤。