Internally cooled turbine 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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F01D 518

Patent

active

052882071

ABSTRACT:
A turbine airfoil having a baffleless cooling passage for directing cooling fluid toward a trailing edge is disclosed. Various construction details are developed which provide axially oriented, interrupted channels for turning a flow of cooling fluid from a radial direction to an axial direction. In a particular embodiment, a turbine airfoil has a cooling passage including a plurality of radially spaced walls, a plurality of radially spaced dividers downstream of the walls, and a plurality of radially spaced pedestals positioned axially between the walls and dividers. The walls and dividers define channels having an axial interruption permitting cross flow between adjacent channels. The cross flow minimizes the adverse affects of a blockage within a subchannel between adjacent walls. The pedestals are aligned with the subchannels such that cooling fluid exiting a subchannel impinges upon the pedestal.

REFERENCES:
patent: 3934322 (1976-01-01), Hauser et al.
patent: 4278400 (1981-07-01), Yamarik et al.
patent: 4407632 (1983-10-01), Liang
patent: 4515523 (1985-05-01), North et al.
patent: 4601638 (1986-07-01), Hill et al.
patent: 4752186 (1988-06-01), Liang
patent: 4753575 (1988-06-01), Levengood et al.
patent: 5102299 (1992-04-01), Frederick

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