Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Radial flow devices
Reexamination Certificate
2006-05-23
2006-05-23
Look, Edward K. (Department: 3745)
Fluid reaction surfaces (i.e., impellers)
Specific blade structure
Radial flow devices
Reexamination Certificate
active
07048509
ABSTRACT:
In the axial turbine according to the present invention, a nozzle blade1and/or a movable blade5has a profile in which a throat-pitch ratio “s/t” is maximized at a blade-central portion in height, wherein “s” being a shortest distance between a rear edge of a nozzle blade (movable blade) and a back side of another nozzle blade that is adjacent to the nozzle blade, and “t” being a pitch of the nozzle blades disposed in the row, minimized in a position between the blade-central portion in height and a blade-root portion and increased from a minimized value to the blade-root portion. This structure enables to provide the axial turbine, which permits to control flow distribution of the working fluid in the height direction of the blade in the passage between the blades of a turbine nozzle unit and a turbine movable nozzle and reduce the blade profile loss and the secondary flow loss at the blade-root portion, thus making a further improvement in the turbine stage efficiency.
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Imai Kenichi
Kawasaki Sakae
Tanuma Tadashi
Tominaga Junichi
Kabushiki Kaisha Toshiba
Kershteyn Igor
Look Edward K.
Oblon & Spivak, McClelland, Maier & Neustadt P.C.
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