Rotary kinetic fluid motors or pumps – With means for re-entry of working fluid to blade set – Radial flow runner portion guides re-entry working fluid
Reexamination Certificate
2005-01-06
2008-03-04
Look, Edward K. (Department: 3745)
Rotary kinetic fluid motors or pumps
With means for re-entry of working fluid to blade set
Radial flow runner portion guides re-entry working fluid
C415S058600, C415S173100, C415S914000
Reexamination Certificate
active
07338251
ABSTRACT:
A turbo compressor comprising a driving motor, an impeller to be rotated by the driving motor, a second gas suction part through which gas is introduced into the impeller, and a discharger through which the gas is discharged from the impeller, the turbo compressor comprises a shroud provided between the gas suction part and the gas discharger and spaced from a blade of the impeller; and a plurality of channels provided on the shroud and inclined toward the gas discharger along a rotating direction of the impeller. With this configuration, the present invention provides a turbo compressor in which compression efficiency is increased by eliminating a backflow and a leakage flow.
REFERENCES:
patent: 3893787 (1975-07-01), Jones
patent: 5555956 (1996-09-01), Voss et al.
patent: 6554568 (2003-04-01), Fledersbacher et al.
patent: 6582189 (2003-06-01), Irie et al.
patent: 6-193596 (1994-07-01), None
patent: 10-141293 (1998-05-01), None
patent: 2000-3085 (2000-01-01), None
patent: 2000-65622 (2000-11-01), None
patent: 2001-81648 (2001-08-01), None
patent: 2001-81649 (2001-08-01), None
Chinese Patent Office Action issued with respect to Chinese Application No. 2004100593342, which corresponds to the above-reference application.
Kim Cheol-woo
Ro Soo-hyuk
Look Edward K.
White Dwayne J
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