Turbine blade outer air seal with optimized cooling

Rotary kinetic fluid motors or pumps – Bearing – seal – or liner between runner portion and static part – Between blade edge and static part

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Details

415115, F01D 520

Patent

active

053759737

ABSTRACT:
This disclosure describes a cooling and manufacturing enhancement for gas turbine engine outer air seals. The invention provides convective cooling in a counter-flow array, internal heat transfer augmentation through the use of boundary layer trip-strips, coolant Mach number control through the use of tapered convective channels, inter-segment purge without additional secondary cooling air, and is castable.

REFERENCES:
patent: 4013376 (1977-03-01), Bisson et al.
patent: 5205115 (1993-04-01), Plemmons
patent: 5219268 (1993-06-01), Johnson

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