órgão de travamento para dispositivo de fixação de setores de anel sobre um cárter de turbomáquina de aeronave, dispositivo de fixação de setores de anel sobre um cárter de turbomáquina de aeronave,turbina de turbomáquina de aeronave, e turbomáquina de aeronave.

摘要

A unit locking a ring sector attachment device onto an aircraft turbomachine casing, the unit including two clamping arms connected to each other at their aft ends by a connecting arm extending approximately parallel to the general direction between the two clamping arms. The unit also includes a passage enabling gripping of the unit on each side of a fictitious median plane orthogonal to the circumferential direction, each passage being formed in the connecting arm, extending along a direction line approximately parallel to the direction between the arms.