Structural reinforcement strut for gas turbine case

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

Patent

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Details

F01D 25/28 (2006.01) B23K 31/02 (2006.01) F01D 25/24 (2006.01) F02K 1/80 (2006.01)

Patent

CA 2701405

A gas turbine engine case having a working fluid flow, includes inner and outer case portions defining an annular duct for directing the working fluid flow, and a plurality of struts positioned within the annular duct and extending between the inner and outer case portions. The struts are welded to the inner and outer case portions with a first weld along a peripheral line of the respective struts and with second weld, of fillet type, in selected locations for additionally connecting a portion of each strut to the respective inner and outer case portions.

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