Turbine rotor blade groove entry slot lock structure

Fluid reaction surfaces (i.e. – impellers) – Specific working member mount – Blade received by continuous circumferential channel

Reexamination Certificate

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Details

C416S215000, C416S218000, C029S889100, C029S889210

Reexamination Certificate

active

07901187

ABSTRACT:
A blade lock structure for blading an axial flow turbine having a rotor and blades. The blades are inserted into an undercut blade groove of the rotor providing a positive lock between the blades and the rotor. The lock structure includes an entry slot located in the blade groove for receiving the blades for insertion to the undercut blade groove, and an insert space axially extending from the entry slot. The insert space defines a radially extending longitudinal axis. An insert piece is located in positive-locking relationship with the insert space, and a lock screw threadably engages between the insert piece and a closing blade inserted to the entry slot.

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