Blade outer air seal support cooling air distribution system

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

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Details

F01D 11/08 (2006.01) F01D 9/00 (2006.01) F01D 25/12 (2006.01) F01D 25/24 (2006.01) F01D 25/28 (2006.01) F02C 7/18 (2006.01) F02C 7/28 (2006.01)

Patent

CA 2712758

A blade outer air seal (BOAS) of a gas turbine engine has a segmented support ring to support a segmented turbine shroud. The support ring has a cooling air distribution system which includes a plurality of inlet cavities extending axially and inwardly to communicate with an inner cooling air passage within the respective support segments. The inlet cavities each are formed with two recesses defined in respective adjacent two support segments.

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