Axial serpentine cooled airfoil

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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416 96R, 415116, F01D 508

Patent

active

060992522

ABSTRACT:
A gas turbine engine airfoil includes an axial serpentine cooling circuit therein. A plurality of the serpentine circuits are preferably stacked in a radial row along the airfoil trailing edge for cooling thereof.

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patent: 5902093 (1999-10-01), Liotta et al.
patent: 5967752 (1999-10-01), Lee et al.
patent: 5997251 (1999-12-01), Lee

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