Laminated airfoil and method for turbomachinery

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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415115, F01D 518

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active

043470378

ABSTRACT:
Improved structure and method for an internally cooled, laminated stator or turbine blade for turbomachinery includes internal cooling passage configurations within each lamina which promote different forms of cooling of the internal or external surfaces of the blade.

REFERENCES:
patent: 3867068 (1975-02-01), Corsmeier et al.
patent: 4040767 (1977-08-01), Dierberger et al.
patent: 4203706 (1980-05-01), Hess
patent: 4221539 (1980-09-01), Corrigan
patent: 4270883 (1981-06-01), Corrigan

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