Gas turbine engine combustor with improved cooling

Details Gas turbine engine combustor with improved cooling Gas turbine engine combustor with improved cooling

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/06 (2006.01) F02C 7/12 (2006.01) F23R 3/42 (2006.01)

Patent

CA 2551539

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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