Shroud hanger with diffused cooling passage

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

Patent

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Details

F01D 11/08 (2006.01) F01D 25/14 (2006.01) F01D 25/24 (2006.01)

Patent

CA 2742004

A shroud hanger (44) for a gas turbine engine has an arcuate body (52) with opposed inner and outer faces and opposed forward and aft ends, a channel having at least one cooling passage (74) therein which includes: (a) a generally axial ly-aligned channel (76) extending through the body, the channel having one end open to an exterior of the body; and (b) a generally radially-aligned diffuser (78) extending through the inner face and intersecting the channel.

L'invention concerne un dispositif de suspension de carénage (44) pour un moteur à turbine à gaz, comprenant un corps courbe (52) présentant des faces intérieure et extérieure opposées et des extrémités avant et arrière opposées, un canal comprenant au moins un passage de refroidissement (74), comprenant : (a) un canal aligné essentiellement axialement (76) qui s'étend à travers le corps, le canal présentant une première extrémité ouverte vers l'extérieur du corps ; et (b) un diffuseur aligné essentiellement radialement (78) qui s'étend à travers la face intérieure et qui coupe le canal.

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