Rotor blade trailing edge assemby and method of use

Details Rotor blade trailing edge assemby and method of use Rotor blade trailing edge assemby and method of use

2011-04-05

2011-04-05

Look, Edward (Department: 3745)

Fluid reaction surfaces (i.e., impellers)

Specific blade structure

Tined or irregular periphery

C416S232000, C416S23600R

Reexamination Certificate

active

07918653

ABSTRACT:
A method of assembling a rotor blade for a turbine is provided that includes forming a rotor blade trailing edge by coupling a suction side terminus to a pressure side terminus and positioning a trailing edge assembly between the suction side terminus and the pressure side terminus, the trailing edge assembly having a varying cross-section.

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