| 摘要 |
A locking blade 100 for a rotor can include an airfoil portion 126 with a root 122 from which a tongue extends 123. Opposed bucket segments 111, 113 can engage the tongue 123 and can be retained in a longitudinal direction of the blade by a fastener 130, such as a pin, that can extend through holes 119 in the segments 111, 113 and tongue 123. Tines 127 parallel to and on opposite sides of the tongue 123 can extend from the root 122 and include holes 129 through which the fastener 130 can extend, the bucket segments 111, 113 extending between respective tines 127 and the tongue 123. The structure 100 can eliminate an assembly gate in a rotor. |
