The invention relates to a comprehensive performance
verification method for a wear-resistant layer of a
turbine blade, and belongs to the technical field of
turbine blades, the comprehensive performance
verification method comprises a melting performance test, a pressure-resistant performance test, a wear-resistant performance test, a high-temperature
hardness test and a tension shear test, and the melting performance test is performed on a
welding rod made of a first material; the first wear-resistant layer made of the first material is subjected to a
pressure resistance test, the second wear-resistant layer and the third wear-resistant layer made of the first material are subjected to a
wear resistance test, the fourth wear-resistant layer made of the first material is subjected to a high-temperature
hardness test, and the blade crown wear-resistant layer made of the first material is subjected to a tension shear test. The device has the beneficial effects that a fusion performance test, a
pressure resistance test, a
wear resistance test, a high-temperature
hardness test and a tension shear test are carried out on the
welding rod made of the first material, so that the comprehensive performance test on the
welding rod made of the first material is realized, and whether the welding rod made of the first material can be used for
processing a blade or not is judged; and the
machining quality and safety of the blade are ensured.