The application belongs to the technical field of strength test of single lug joint of vertical
tail wall plate root of an
airplane, and particularly relates to a
radial compression test loading structure of a single lug joint shaft hole of a vertical
tail wall plate root of an
airplane, when strength test is performed by using the
radial compression test loading structure, a test
machine can apply a
pressure load on a wall surface of a loading pressure platform, the
pressure load can be transmitted to a shaft hole of a single lug joint of a single lug joint test piece through a support
bushing and a loading shaft, a
radial compression load is applied in the shaft hole of the single lug joint, in the process, two support bushings can support the single lug joint of the single lug joint test piece from two sides, two support plates can support a transition section of the single lug joint test piece from two sides,
lateral deviation of the single lug joint test piece is prevented, and the two support bushings and the support plates can follow the loading pressure platform to follow the support, the stress environment of the single lug joint can be well ensured, and the accuracy of a test result can be ensured.