The utility model discloses an aero-engine
directional solidification blade structure integrity auxiliary detection device, and belongs to the technical field of blade detection. The aero-engine
directional solidification blade structure integrity auxiliary detection device comprises a blade profile mold and a lineation sample plate, the blade profile mold comprises a blade basin, a blade back and a blade root, an
airflow channel is arranged in the blade basin, and the lineation sample plate is fixedly attached to the blade basin, the blade back and the blade root. In order to solve the problems that a geometric included angle between a
grain boundary and a Z axis is difficult to accurately calculate under a visual condition, an inspector usually judges according to subjective experience, and
mass escape is possibly caused, after a plurality of lineation sample plates are fixed, scribed lines parallel to the Z axis are marked near the position where the
grain boundary included angle needs to be measured, and finally, a
protractor is used for measuring the
grain boundary included angle. And measuring the grain boundary of which the included angle needs to be measured, reading the numerical value alpha of the included angle of the grain boundary according to the scribed line of the
protractor, and recording the numerical value alpha, wherein the scribed line parallel to the Z axis corresponds to the zero position of the
protractor.