| 摘要 |
The rotor (10) has rotating blades (12) equipped with a rotor base body (16). A cooling air channel (22) is provided radially below a blade platform of the rotating blades, where the cooling air channel is extended from a high pressure side (HD) to a low pressure side (ND) of the rotating blades. An inclination of a main extension axis (H) of the cooling air channel has a sign, same as an inclination of a main extension axis (R) of a radial inner flow channel border of the rotor. An independent claim is also included for a method for manufacturing rotor for a turbo-machine. |
