Vane wheel for radial turbine

Fluid reaction surfaces (i.e. – impellers) – Rotor having flow confining or deflecting web – shroud or... – Radially extending web or end plate

Reexamination Certificate

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Reexamination Certificate

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06942460

ABSTRACT:
A radial turbine impeller is provided, comprising a circular main disk provided with a plurality of blades, each having a negative pressure surface and a positive pressure surface; scallops being formed by cutting off the main disk between the negative pressure surface of the one blade and the positive pressure surface of the other blade adjacent to the one blade, respectively; wherein a minimum radius portion of the scallop having a minimum distance between a center of the circular main disk and the edge of the scallop is positioned closer to the positive pressure surface so that the scallop is asymmetric between the negative pressure surface of the one blade and the positive pressure surface of the other blade adjacent thereto.

REFERENCES:
patent: 3040670 (1962-06-01), Schenck et al.
patent: 4659288 (1987-04-01), Clark et al.
patent: 5061154 (1991-10-01), Kington
patent: 5605444 (1997-02-01), Paton et al.
patent: 0184934 (1986-06-01), None
patent: 61-39402 (1986-03-01), None
patent: 61-142301 (1986-06-01), None
patent: 4-52504 (1992-05-01), None
patent: 5-502711 (1993-05-01), None
patent: 10131704 (1998-05-01), None
patent: 91/09209 (1991-06-01), None

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