Cooled 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

Reexamination Certificate

active

07104757

ABSTRACT:
The invention relates to a turbine blade which has a nose cavity in the region of a leading edge, it being possible for the leading edge to be cooled by impingement cooling, which has an inner cavity at least partly of meander-shaped design, and which has a crown pocket as cavity in the region of the blade tip, which crown pocket is connected to the nose cavity, so that the cooling of the turbine blade is improved.

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patent: 32 34 906 (1983-06-01), None
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patent: 1 022 434 (2000-07-01), None

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