A blade-disk assembly (200) for a gas turbine (100) includes a blade (230) having a root part (235), a disk (210) having a disk slot (213), into which the root part (235) is inserted, and a fixing block (250) inserted into a block assembly groove (237) of ...

The aircraft gas turbine has a fan in the inlet flow area of the aircraft gas turbine, where the fan is rotatable around an engine axis. The fan has multiple fan blades (30). Each fan blade is placed on a hub (29) by a blade foot (31), where the hub is rot...