| 摘要 |
An improved connection of blades (12) on a rotor disc (22) of a gas turbine, of the type in which a root (10) of each blade (12) is inserted in a seat (20) of the disc (22) which is complementary to the blade, wherein the root (10) is in the shape of an overturned isosceles triangle, with the two sides which converge at the base each having a grooved profile such as to form a series of teeth (14) and with a lower end (16) of the root (10) which is formed by the joined connection of the two lower teeth (14) of the two sides of the root (10), the teeth (14) of the root (10) corresponding to grooves (24) in the seat (20) and the lower end (16) of the root (10) corresponding to an end groove (26) in the seat (20). This series of grooves (24) extends along a line which is inclined relative to the axis of the seat (20) by an angle beta 1 of between 17 DEG and 23 DEG , and the grooves (24) have straight sides with inclinations relative to the axis of the seat (20) of angles alpha 1 and alpha 2, wherein alpha 1 is between 42 DEG and 48 DEG whereas alpha 2 is between 94 DEG and 100 DEG . <IMAGE> |
