Vane for a stator of a variable-geometry turbine, in particular for aeronautical engines

This Application claim priority under 35 U.S.C. §119 of Italian application number TO2001A 000445, filed May 11, 2001 in Italy. A vane for a stator of a variable-geometry turbine, in particular for aeronautical engines, has an airfoil profile and a pair of hinge portions, which are carried by the airfoil profile and enable the airfoil profile to be coupled to a support structure of the stator so as to be rotatable about an axis of adjustment; the vane also has internal channels that allow a flow of air to pass through in order to cool the hinge portions.