High-pressure turbine vane including a cavity under a squealer tip

A method for manufacturing a vane of a turbine engine comprising a pressure-face wall and a suction-face wall spaced apart from one another, this vane comprising a tip with:

• a bottom wall extending from the pressure-face wall to the suction-face wall, the pressure-face wall and the suction-face wall each comprising a free edge extending beyond this bottom wall to delimit, together with this bottom wall, a squealer shape at the tip of the vane;
• a partition wall extending from the pressure-face wall to the suction-face wall and spaced apart from the bottom wall to delimit, together with this bottom wall, a cavity under the squealer tip;
• the method including:
• moulding to form at least the pressure-face wall, the suction-face wall, and the partition wall;
• and
• forming the bottom wall directly on the pressure-face wall and the suction-face wall formed by the moulding using an additive manufacturing method by adding metal material,
• wherein the forming the bottom wall using the additive manufacturing method includes orienting the vane such that a spanwise axis of the vane extends in a horizontal direction during the additive manufacturing.