Turbine components

Fluid reaction surfaces (i.e. – impellers) – With heating – cooling or thermal insulation means – Changing state mass within or fluid flow through working...

Reexamination Certificate

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Details

C416S09600A, C416S09700R, C415S115000

Reexamination Certificate

active

07137781

ABSTRACT:
A turbine component, such as a turbine blade1, 21, has a coolant supply passage4, 24and a cooling chamber3, 23connected by an injection passage5, 25. The cooling chamber3, 23includes flow guides in the form of vanes7, 8or grooves37which act to create a coolant flow in a spiral direction. Thus, there is limited coolant flow impingement and greater cooling effect to allow the turbine component to operate at higher temperatures.

REFERENCES:
patent: 3373970 (1968-03-01), Brockmann
patent: 4505639 (1985-03-01), Groess et al.
patent: 5002460 (1991-03-01), Lee
patent: 5603606 (1997-02-01), Glezer
patent: 6874988 (2005-04-01), Tiemann
patent: 1197636 (2002-04-01), None
patent: WO-02/27146 (2002-04-01), None

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