Rotor blade shroud segment

Details Rotor blade shroud segment Rotor blade shroud segment

F - Mech Eng,Light,Heat,Weapons

01

D

170/76

F01D 5/22 (2006.01) F01D 11/08 (2006.01) F01D 25/24 (2006.01)

Patent

CA 2031086

13DV-8824 ROTOR BLADE SHROUD SEGMENT Abstract of the Disclosure A shroud segment adapted to mount to the casing of the turbine or compressor of a gas turbine engine includes opposed ends, an inner face, an outer face and forward and aft side mounting rails. The forward and aft side mounting rails are each formed with a pair of substantially T-shaped relief slots having a straight stem section extending inwardly from the outer face of the shroud body toward the inner face, and an arcuate-shaped head section connected to the stem section which reduces stress concentrations at the base of the stem section of the relief slot.

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