Thermally high-stressed cooled component, particularly a blade f

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

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416231R, 416241B, F01D 518

Patent

active

040676625

ABSTRACT:
A thermally highly stressed, cooled component, more particularly, a blade for turbine engines, and a method for manufacturing the blade. A component of the above-mentioned type in which a central supporting core formed of a solid material has connected thereto several short, radially outwardly projecting ridges which, in turn, carry an outer shroud concentrically encompassing the supporting core, and which is made of a through-porous material, whereby the supporting core, ribs, and outer shroud are cast in a single piece.

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patent: 3114961 (1963-12-01), Chambers et al.
patent: 3529902 (1970-09-01), Emmerson
patent: 3656863 (1972-04-01), DeFeo
patent: 3706508 (1972-12-01), Moskowitz et al.

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