Turbine engline, such as for example an aircraft turbojet engine or a turboprop engine

A turbine engine such as for example an aircraft turbojet engine or a turboprop engine, comprising at least one element comprising a wall, at least a first yoke, also called a main yoke, for example attached to the beam used for fixing the turbine engine onto a shroud of an aircraft, and at least a second yoke, also called an auxiliary yoke, clearance mounted for example on the beam, with said yokes extending substantially perpendicularly to said wall, with said auxiliary yoke being adapted to take up stress in case of deformation of the element and/or in case of breakage of the main yoke, comprising a thermal protection member surrounding the auxiliary yoke only, with said thermal protection member comprising a base flexibly supported on the wall of the element, with said base matching the shape of said wall and at least one covering part which surrounds said auxiliary yoke.