Multipart gas turbine blade

Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Radial flow devices

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Details

416213R, 416241R, 2988921, 2988922, F01D 514

Patent

active

053184068

ABSTRACT:
A turbine blade comprises an airfoil/shank having a shank region and an airfoil region extending upwardly therefrom and two dovetail/platforms bonded thereto. The first dovetail/platform has a first dovetail region bonded to a first side of the shank region of the airfoil/shank, with a first platform region extending outwardly from the first dovetail region. The second dovetail/platform has a second dovetail region bonded to a second side of the shank region of the airfoil/shank and a second platform region extending outwardly from the second dovetail region in a direction generally opposite to that of the first platform region.

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