High-pressure turbine stator ring for a turbine engine

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

Patent

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F01D 9/04 (2006.01) F01D 11/18 (2006.01) F01D 25/24 (2006.01)

Patent

CA 2276238

The present invention relates to the high-pressure turbine stator ring of a turbo engine that is fastened to the stator by tightening means that limit leaks to a minimum. These means mainly comprise a tightening grip (40) that grips the curved section of a downstream leg (35V) of each spacer section (30) that is fastened to the turbine casing (1) of the stator by a curved downstream flange (23V) of each ring section (20). Application to the fastening of the high-pressure turbine stator ring of a turbo engine.

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