Turbine engine and a method for cooling a turbine engine

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

Reexamination Certificate

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C415S116000, C416S09700R

Reexamination Certificate

active

07131813

ABSTRACT:
A turbine engine with a turbine shaft which has a number of disks arranged adjacent to one another, to each of which a number of blades are fastened in a star arrangement, wherein these blades can be cooled with at least one coolant which flows through coolant channels inside the blades is provided.

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patent: 6195979 (2001-03-01), Fukuyama
patent: 0 806 544 (1997-11-01), None
patent: 0 900 919 (1999-03-01), None

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