Rotor blade for a rotary machine

Rotary kinetic fluid motors or pumps – Bearing – seal – or liner between runner portion and static part – Between blade edge and static part

Reexamination Certificate

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Details

C415S173600, C416S190000, C416S191000, C416S192000, C416S22300B, C416S243000, C416SDIG004

Reexamination Certificate

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07134838

ABSTRACT:
A rotor blade having a wing and beam construction for a tip shroud is disclosed. Various construction details are developed for providing the shroud with a depression in the shroud and a transition zone that extends from the suction side and pressure side of the airfoil to provide a flow path surface of the shroud. In one detailed embodiment, the tip shroud has a depression generally outwardly of the airfoil and generally following the curve of the pressure and suction sides of the airfoil from the leading edge region to the trailing edge region.

REFERENCES:
patent: 5037273 (1991-08-01), Krueger et al.
patent: 5154581 (1992-10-01), Borufka et al.
patent: 6241471 (2001-06-01), Herron
patent: 6402474 (2002-06-01), Okuno
patent: 6491498 (2002-12-01), Seleski et al.
patent: 6499950 (2002-12-01), Willett et al.
patent: 6805530 (2004-10-01), Urban
patent: 6857853 (2005-02-01), Tomberg et al.
patent: 6890150 (2005-05-01), Tomberg
patent: 6913445 (2005-07-01), Beddard et al.
patent: 2005/0169758 (2005-08-01), Dube et al.
patent: 2005/0169761 (2005-08-01), Dube et al.
patent: 3150526 (1995-09-01), None

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