Split annular ring for turbine engine rotating part

Details Split annular ring for turbine engine rotating part Split annular ring for turbine engine rotating part

F - Mech Eng,Light,Heat,Weapons

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F01D 5/02 (2006.01) F01D 5/10 (2006.01) F01D 11/00 (2006.01) F02C 7/045 (2006.01) F02C 7/20 (2006.01)

Patent

CA 2655916

Jonc annulaire (38) fendu destiné à être monté précontraint élastiquement dans une gorge annulaire (24) d'une pièce tournante (10) de turbomachine et ayant à l'état libre un diamètre supérieur à celui de la gorge (24), caractérisé en ce qu'à l'état libre sans contrainte, les parties d'extrémité (40, 42) du jonc (38) sont des arcs de cercle ayant un rayon de courbure sensiblement égal à celui de la gorge annulaire (24).

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