Gas turbine engine combustor with improved cooling

Power plants – Combustion products used as motive fluid – Combustion products generator

Reexamination Certificate

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C060S754000, C060S760000

Reexamination Certificate

active

07451600

ABSTRACT:
A gas turbine engine combustor liner having a plurality of holes defined therein for directing air into the combustion chamber. The plurality of holes provide improved cooling efficiency in regions of the combustor dome corresponding to predetermined hotspots.

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