Cooled gas turbine blade

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

Patent

active

054315379

ABSTRACT:
A hollow air cooled airfoil blade (10) castable with a single pull core and having internal trip strips (28) at the leading edge. Parallel ribs (16,18) extend from the pressure side (12) of the blade to the suction side (14). A parting line (32) passes through the most forward point (34) of the airfoil, this being located on the suction side of the leading edge (36). The trip strips stop short of the parting line.

REFERENCES:
patent: 3627443 (1971-12-01), Pirzer
patent: 4416585 (1983-11-01), Abdel-Messeh
patent: 4514144 (1985-04-01), Lee
patent: 5052889 (1991-10-01), Abdel-Messeh
patent: 5232343 (1993-08-01), Butts
patent: 5259730 (1993-11-01), Damlis et al.

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