A baffle insert for an internally cooled airfoil, the baffle insert comprising: a liner having a continuous perimeter formed to shape a hollow body having a first end and a second end; a divoted segment (28,30) of the hollow body positioned between the first end and the second end; and a plurality of cooling holes (32,34) positioned on the divoted segment to aim cooling air exiting the baffle insert, wherein the divoted segment (28,30) comprises an elongate, longitudinal depression in the hollow body extending between the first end and the second end, wherein the depression comprises: a first curved segment having a first column of cooling holes; a second curved segment having a second column of cooling holes; and an elbow segment connecting the first curved segment with the second curved segment and having a third column of cooling holes, wherein the first and second curved segments (30B, 30C) are curved to direct air through the first and second columns of cooling holes at angles oblique to an interior surface of the airfoil, and characterised in that: the elbow segment is curved to direct air through the third column of cooling holes at an angle normal to the profile of the baffle and the interior surface of the airfoil, and the first and second curved segments (30B, 30C) and the elbow segment are curved to focus cooling air from the first, second and third columns of cooling holes such that the cooling air from the first, second and third columns of cooling holes intersects at a common location. a liner having a continuous perimeter formed to shape a hollow body having a first end and a second end; a divoted segment (28,30) of the hollow body positioned between the first end and the second end; and a plurality of cooling holes (32,34) positioned on the divoted segment to aim cooling air exiting the baffle insert, wherein the divoted segment (28,30) comprises an elongate, longitudinal depression in the hollow body extending between the first end and the second end, wherein the depression comprises: a first curved segment having a first column of cooling holes; a second curved segment having a second column of cooling holes; and an elbow segment connecting the first curved segment with the second curved segment and having a third column of cooling holes, a first curved segment having a first column of cooling holes; a second curved segment having a second column of cooling holes; and an elbow segment connecting the first curved segment with the second curved segment and having a third column of cooling holes, wherein the first and second curved segments (30B, 30C) are curved to direct air through the first and second columns of cooling holes at angles oblique to an interior surface of the airfoil, and characterised in that: the elbow segment is curved to direct air through the third column of cooling holes at an angle normal to the profile of the baffle and the interior surface of the airfoil, and the first and second curved segments (30B, 30C) and the elbow segment are curved to focus cooling air from the first, second and third columns of cooling holes such that the cooling air from the first, second and third columns of cooling holes intersects at a common location. the elbow segment is curved to direct air through the third column of cooling holes at an angle normal to the profile of the baffle and the interior surface of the airfoil, and the first and second curved segments (30B, 30C) and the elbow segment are curved to focus cooling air from the first, second and third columns of cooling holes such that the cooling air from the first, second and third columns of cooling holes intersects at a common location.