Turbine engine vane baffle

An assembly for a turbine engine, comprising:

• at least one airfoil extending spanwise from an airfoil base end to an airfoil tip end, the airfoil extending longitudinally from an airfoil leading edge to an airfoil trailing edge, the airfoil extending laterally between an airfoil first side and an airfoil second side with the airfoil second side meeting the airfoil first side at the airfoil leading edge and the airfoil trailing edge, and an airfoil cavity projecting spanwise into the airfoil from the airfoil tip end towards the airfoil base end;
• and
• a baffle disposed in the airfoil cavity with a passage formed between the baffle and a wall of the airfoil, the baffle extending longitudinally from a baffle end to a baffle trailing edge, the baffle extending laterally between a baffle first side and a baffle second side with the baffle second side meeting the baffle first side at the baffle trailing edge, the baffle extending spanwise from a baffle base end to a baffle tip end, the baffle including a first sidewall, a second sidewall and a baffle cavity, the first sidewall forming the baffle first side longitudinally along the baffle cavity, the second sidewall forming the baffle second side longitudinally along the baffle cavity, the first sidewall meeting the second sidewall at an interface spanwise along the baffle trailing edge, the first sidewall longitudinally overlapping and laterally abutting against the second sidewall at the interface, and the first sidewall bonded to the second sidewall at the interface.