Quench jet arrangement for annular rich-quench-lean gas...

Details Quench jet arrangement for annular rich-quench-lean gas... Quench jet arrangement for annular rich-quench-lean gas...

F - Mech Eng,Light,Heat,Weapons

23

R

F23R 3/04 (2006.01) F23R 3/34 (2006.01) F23R 3/42 (2006.01)

Patent

CA 2644837

An outer liner of a combustor of a gas turbine engine includes a plurality of liner regions arranged adjacent one another and separated by boundary lines; and a plurality of air admission holes formed in the liner regions. The air admission holes within each liner region form a V-pattern.

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