Engine loading simulated sample for static test of airplane

The utility model belongs to the field of aviation machinery, and in particular relates to an engine loading simulated sample for a static test of an airplane. The engine loading simulated sample comprises a loading plane [1], a front disc [2], a box-shaped part [3], a bearing shaft [4] and a back disc [5], wherein the loading plane [1] is fixed on the front disc [2], the front disc [2] is fixed on the bearing shaft [4], the box-shaped part [3] is close to the front disc [2] and is fixed on both sides of the bearing shaft [4], the back disc [5] is fixed on the tail of the bearing shaft [4], and main shaft necks [6] are arranged on both ends of the box-shaped part [3]. According to the utility model, through verification of all-structure-size structural static test of a series of airplanes, the engine loading simulated sample has the characteristics of low manufacturing cost, simple installation and convenient loading implementation, and the like, and is convenient for applying engine and propeller loads, the