Turbine blade

Rotary kinetic fluid motors or pumps – With passage in blade – vane – shaft or rotary distributor...

Reexamination Certificate

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Details

C416S09700R

Reexamination Certificate

active

06945750

ABSTRACT:
A turbine blade for a gas turbine has a hollow airfoil extending from a platform. There is a fillet between the airfoil and the platform, both on the pressure side and on the suction side of the airfoil. The fillet contains a cooling bore extending along part of the length of the fillet, having a first end communicating with the interior of the turbine blade for receiving a gaseous coolant and a second end communicating with the exterior of the turbine blade. The cooling may be formed by electro-discharge machining.

REFERENCES:
patent: 4012167 (1977-03-01), Noble
patent: 4040767 (1977-08-01), Dierberger et al.
patent: 4863348 (1989-09-01), Weinhold
patent: 5340278 (1994-08-01), Magowan
patent: 5382135 (1995-01-01), Green
patent: 6120249 (2000-09-01), Hultgren et al.
patent: 6354797 (2002-03-01), Heyward et al.
patent: 6644920 (2003-11-01), Beeck et al.
patent: 2002/0076324 (2002-06-01), Abuaf et al.
patent: 26 43 049 (1977-04-01), None
patent: 100 59 997 (2002-06-01), None
patent: 11-247606 (1999-09-01), None

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