GAS TURBINE BLADE AND GAS TURBINE WITH THE BLADE

The invention relates to a gas turbine blade and a gas turbine with the blade. The rotating blade for a gas turbine (5) is provided with: a root (17) configured to be coupled to a disc of the gas turbine (5) which rotates about an axis (A) of the gas turbine (5); a platform (20) coupled to the root (17); an airfoil (18) extending from the platform (20) and provided with a tip (23) radially opposite to the root (17) or the platform (20); the airfoil (18) comprising a leading edge (27), a trailing edge (28), a pressure side (25) and a suction side (26); at least one snubber (22; 22a, 22b) projecting from the suction side (26) and/or the pressure side (25); the snubber (22; 22a, 22b) being shaped so as to create a centripetal force towards the root (17) opposing the centrifugal force generated during the rotation of the disc to which the blade (15) is coupled. 本发明涉及用于燃气涡轮机的叶片和包括所述叶片的燃气涡轮机。用于燃气涡轮机（5）的旋转叶片配有：根部（17），其构造成耦接到燃气涡轮机（5）的绕燃气涡轮机（5）的轴线（A）旋转的盘；耦接到根部（17）的平台（20）；从平台（20）延伸并设有与根部（17）或平台（20）径向相对的末端（23）的翼型件（18）；翼