Turbine blade which can be subjected to a hot gas flow

Details Turbine blade which can be subjected to a hot gas flow Turbine blade which can be subjected to a hot gas flow

1999-03-04

2000-03-21

Look, Edward K.

Fluid reaction surfaces (i.e., impellers)

With heating, cooling or thermal insulation means

Changing state mass within or fluid flow through working...

416 96R, 416 96A, 416241R, 416241B, 415115, F01D 518

Patent

active

060395370

ABSTRACT:
A turbine blade which can be subjected to a hot gas flow includes a substrate, at least one interior space and a plurality of bores leading from the interior space out of the substrate. The substrate is at least partly covered by a heat-insulating-layer system at a suction side and/or a pressure side. At least one of the bores is closed by the heat-insulating-layer system and at least one further bore is open for developing film cooling.

REFERENCES:
patent: 5030060 (1991-07-01), Liang

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