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.