Sector of a turbine stator for a turbine of an aircraft turbomachine

Abstract

A sector of a turbine stator for a turbine of an aircraft turbomachine, the sector having an outer platform and an inner platform which are coaxial along an axis. The sector further includes at least one blade which connects the outer and inner platforms together, with the blade being variable-pitch about an axis of rotation of the blade. The blade can include an aerodynamic body delimited radially by a head and a root, the head being placed with a first functional clearance in an opening of the outer platform, the root being placed with a second functional clearance in a cavity of the inner platform, the axis of rotation of the blade being located downstream of the head and the root.

Dependencies are inferred from the claim text.