The invention relates to a
coating cutting tool and a manufacturing method thereof. The
coating cutting tool is composed of a base material and a hard material
coating, and the base material is selected from
cemented carbide,
cermet,
ceramic, cubic
boron nitride (cBN),
polycrystalline diamond (PCD) or
high speed steel (HSS), wherein the hard material coating comprises a (Ti,Al)N layer stack (L) of alternately stacked (Ti,Al)N sublayers , said layer stack (L) is characterized in that: - the total
atomic ratio of Ti:Al in said (Ti,Al)N layer stack (L) is in the range of 0.33:0.67 to 0.67:0.33; - The
total thickness of the (Ti,Al)N layer stack (L) is in the range of 1 μm to 20 μm; - in the (Ti,Al)N layer stack of alternately stacked (Ti,Al)N sublayers Each individual (Ti,Al)N sublayer within (L) has a thickness in the range of 0.5 nm to 50 nm; Each individual (Ti,Al)N sublayer within the stack (L) differs from the immediately adjacent (Ti,Al)N sublayer in the
atomic ratio Ti:Al; On the thickness of the (Ti, Al)N layer stack (L), from the interface of the (Ti, Al)N layer stack (L) aligned toward the substrate to the at the interface of the (Ti,Al)N layer stack (L) in the direction of the outer surface of the coating, the
Al content increases and the Ti content decreases; - at the (Ti,Al)N layer perpendicular to the
substrate surface , Al)N layer stack (L), from the interface of the (Ti,Al)N layer stack (L) aligned towards the substrate to the layer aligned towards the outside of the coating At the interface of said (Ti,Al)N layer stack (L) in the direction of the surface, the
residual stress σ drops by an amount of at least 150 MPa to at most 900 MPa, whereby applying the sin based on (200) reflection 2 Ψ method to measure the
residual stress σ by X-
ray diffraction; Said
residual stress σ in a portion of a thickness of at least 100 nm to at most 1 μm from the interface of the layer stack (L) is in the range of 0 MPa to +450 MPa.