Attenuating shroud support

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 11/18 (2006.01)

Patent

CA 2048779

Patent 13LN-1940 ABSTRACT A shroud support for a gas turbine engine includes a mounting flange mountable to a casing, a hanger for supporting a turbine shroud, and an annular coupling joining the mounting flange to the hanger. The coupling includes a plurality of circumferentially spaced apertures defining a plurality of beams therebetween, with the beams being sized and configured for attenuating radial distortion from the mounting flange transmitted to the hanger. In a preferred embodiment of the invention, the coupling includes a frustum which includes the apertures and beams.

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