Blade of a turbomachine with block-wise defined profile...

Rotary kinetic fluid motors or pumps – Working fluid passage or distributing means associated with... – Plural distributing means immediately upstream of runner

Reexamination Certificate

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Details

C416S243000, C416SDIG004

Reexamination Certificate

active

11510826

ABSTRACT:
A turbomachine blade with a profile skeleton line extending along a meridional flow line, the blade being radially divided into at least three zones (Z0, Z1, Z2) with profile skeleton lines of each zone (Z0, Z1, Z2) provided in each zone from the respective radially inner to the radially outer boundary to satisfy the equations:α*=α1-αPα1-α2S*=sPSwhereP is any point of the profile skeleton line,α1is angle of inclination at blade leading edge,α2is angle of inclination at blade trailing edge,α* is dimensionless, specific angle of total curvature,S* is dimensionless; specific extension,αPis angle of tangent at any point P of profile skeleton line to central meridional flow line,sPis extension of profile skeleton line at any point P, andS is total extension of profile skeleton line.

REFERENCES:
patent: 4431376 (1984-02-01), Lubenstein
patent: 5312230 (1994-05-01), Oda
patent: 5707206 (1998-01-01), Goto et al.
patent: 6244817 (2001-06-01), Ngo
patent: 6299412 (2001-10-01), Wood
patent: 2324951 (1999-09-01), None
patent: 4243052 (1993-06-01), None
patent: 69820853 (2004-01-01), None
patent: 0661413 (1998-08-01), None
patent: 1106835 (2001-06-01), None
patent: 1106836 (2001-06-01), None

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