MEMBER FOR LOCKING RING SECTORS ON A TURBINE ENGINE CASING, INCLUDING AXIAL PASSAGES FOR GRIPPING SAME

摘要

The invention relates to a locking member (24) for a fastening device for ring sectors on the casing of an aircraft turbine engine, wherein the member includes two clamping arms (28, 30) connected together at the rear end thereof by a connection arm (32) extending substantially parallel to a general spacing direction of the two clamping arms. According to the invention, the member is provided, on either side of a virtual median plane (P2) orthogonal to the circumferential direction, with a passage (42) for gripping the member, each passage being formed through said connection arm (32) and leading into an inter-arm gap (40).