The invention relates to a turbine blade (1) through which a cooling fluid flows, which has a plurality of flow channels (4, 5, 6) arranged adjacently along the outflow direction (2) of a working fluid (3), the flow Inlet holes (7, 8, 9) of channels (4, 5, 6) at the radially inner blade root (10) and outlet holes (11 , 12, 13) extend in such a way that the radial flow component (15) of the resultant cooling fluid flow (14) is practically oriented mainly radially outwards, wherein there is a (2) Look at the flow channel (4) at the front, whose outflow hole (11) is machined in the brushing edge (16) of the turbine blade (1). In addition, at least one trailing channel (5, 6) is provided, in which the combined cooling fluid flow (14) additionally has a local transverse flow component (17), and the outflow holes (12, 13) of the trailing channel Machined in the trailing edge (18) of the turbine blade (1).