Due to the fact that a carbon fiber reinforced polymer composite (CFRP) has the beneficial effects of being high in specific strength, high in specific modulus, light, durable and the like, the carbon fiber reinforced polymer composite (CFRP) becomes an ideal use material in the field of aerospace. Machining defects such as layering, burrs, fiber tearing and hole wall scratching are quite likely to be generated in the CFRP hole making process and seriously influence the strength and the fatigue life of CFRP connection structures. Layering is mainly caused by the fact that the axial force of holes is larger than the interlayer bonding force of CFRP plates during hole machining. The burrs and tearing are mainly caused by obtuse cutting edges of blades. The hole scratching is mainly caused by the interaction between rear cutter faces of tools, cuttings and hole walls. Thus, a welded type blade used for CFRP drilling machining is designed and used for reducing the defects in the CFRP machining process. The blade mainly comprises a blade body 1, a main cutting edge 2, a main front cutter face 3, a first main rear cutter face 4, a second main rear cutter face 5, a first auxiliary cutting edge 6, an auxiliary front cutter face 7, a second auxiliary cutting edge 8, a first auxiliary rear cutter face 9 and a second auxiliary rear cutter face 10.