Transonic blade profiles

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

Reexamination Certificate

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C416SDIG004, C416SDIG004

Reexamination Certificate

active

10861603

ABSTRACT:
The present invention relates to the aerodynamic design of moving blades, pertaining to later stages of axial steam turbines where the inlet flow is non-uniform over the blade height. The claim made herein is a set of six invented transonic blade profiles which can be used to develop various type of 3D twisted blades for axial steam turbine. The aerodynamic characteristics of these 6 base profiles are evaluated herein as a function of stagger angle and pitch/chord ratios.

REFERENCES:
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patent: 3333817 (1967-08-01), Rhomberg
patent: 3565548 (1971-02-01), Fowler et al.
patent: 4695228 (1987-09-01), Purcaru
patent: 5035578 (1991-07-01), Tran
patent: 5192190 (1993-03-01), Ferleger et al.
patent: 5211703 (1993-05-01), Ferleger et al.
patent: 5779443 (1998-07-01), Haller et al.
patent: 6709239 (2004-03-01), Chandraker
patent: 6739838 (2004-05-01), Bielek et al.
patent: 6802695 (2004-10-01), Haller

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