Arrangement for axially securing rotating blades in arotor, and gas turbine having such an arrangement
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[0025]FIG. 3 shows a detail of the end-face plan view of the shaft collar 21, which is formed by a rotor disk 19, of a rotor 23 of a gas turbine. The rotor 23, which is rotatable around the rotational axis 50, has rotor blade retaining slots 12 which are distributed on its outer periphery 52 along the circumference U and extend in the axial direction, into which slots a rotor blade 14, with a blade root 54 which is constructed corresponding to the rotor blade retaining slot 12, in each case can be inserted. A rotor blade 14 is already inserted in the rotor blade retaining slot 12 which is shown in the middle in FIG. 3. As in the case of the prior art which is shown in FIG. 1 and FIG. 2, a projection 58 or widening, with a radially outwardly open encompassing slot 20 therein, which extends in the axial direction, is arranged on an end face of the rotor disk 19 or on an end-face side surface 56 of the shaft collar 21. The encompassing slot 20 for example is arranged radially further i...
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