Turbine blade and gas turbine with such a turbine blade

The invention relates to a turbine blade (63 and 65), comprising a along the blade axis (73 and 75) and a blade is (67 and 69) and a platform (61); the rear is arranged on the blade (67 and 69) and root and transverse of the platform of the blade axis (73 and 75) extends (71). A balsaming of the present invention of the gas turbine (1) oil channel (5) and is far and can simply (87). Therefore according suggested platform (71) through a terminal of the blade (67 and 69) on elastic spring plate (77 and 79) and. The plate is so the gas turbine (1), comprising (3) extended along the gas turbine (1) axis comprises a and an annular cross - section of the movable channel (5) and a working medium (M) (3) is arranged on the first blade layer and axis (7 and 11) and second blade layer (9 and 13,), a blade layer with a certain amount inner ring along the radial direction extending to the flowing channel (5) in according to a turbine blade of the project component (63 and 65).