Gas turbine engine combustor with improved cooling

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

Reexamination Certificate

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C060S804000

Reexamination Certificate

active

07624577

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 a greater cooling air flow in regions intermediate each diffuser pipe than in other areas of the combustor liner.

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