Shroud segment arrangement for gas turbine engines

Details Shroud segment arrangement for gas turbine engines Shroud segment arrangement for gas turbine engines

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 9/04 (2006.01) F01D 11/08 (2006.01) F01D 25/22 (2006.01)

Patent

CA 2649515

The gas turbine engine shroud comprises a plurality of circumferentially-- disposed and concentric shroud segments. Each shroud segment has an arc--shaped platform with opposite ends, each end comprising an inter-segment seal slot, at least one slot extending substantially across each corresponding end and having a lengthwise-variable depth.

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