Turbine blade

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

C415S115000, C415S121300, C415S169100, C416S09600A, C416S09700R

Reexamination Certificate

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07654795

ABSTRACT:
An aerofoil for a gas turbine engine, the aerofoil comprises a leading edge and a trailing edge, pressure and suction surfaces and defines therebetween an internal passage for the flow of cooling fluid therethrough. A particle deflector means is disposed within the passage to deflect particles within a cooling fluid flow away from a region of the aerofoil susceptible to particle buildup and subsequent blockage, such as a cooling passage for a shroud of a blade.

REFERENCES:
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patent: 5827043 (1998-10-01), Fukuda et al.
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patent: 2 262 314 (1993-06-01), None
patent: 2 349 920 (2000-11-01), None

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