Abstract: A method for evaluating damage to a thermal barrier applied to a component made from a metal substrate, the thermal barrier including a sublayer of aluminum and a layer of columnar-structure ceramic material, the sub-layer being positioned between the substrate and the ceramic layer, the method including: a first calibration including selection of a determined number of calibration components that have undergone various degrees of damage, exposing them for a given length of time to radiation, measuring temperature obtained at the surface after the given length of time and establishing a curve connecting an increase in temperature to damage, and a second measuring the damage to the thermal barrier of the component including exposure to the radiation for the length of time, measuring the temperature obtained, and relating the increase in temperature to the calibration curve in order, from the curve, to extract the level of damage.

Abstract: A device for non-destructive in situ inspection of parts of a turbine engine, the device including a stick carrying at its distal end a pivoting finger carrying at one of its ends a blade for supporting an inspection probe, and at its opposite end a skid for bearing against and/or catching on an element of the engine, the skid being movable in a direction parallel to the longitudinal axis of the finger.

Abstract: A method for evaluating damage to a thermal barrier applied to a component made from a metal substrate, the thermal barrier including a sublayer of aluminium and a layer of columnar-structure ceramic material, the sub-layer being positioned between the substrate and the ceramic layer, the method including: a first calibration including selection of a determined number of calibration components that have undergone various degrees of damage, exposing them for a given length of time to radiation, measuring temperature obtained at the surface after the given length of time and establishing a curve connecting an increase in temperature to damage, and a second measuring the damage to the thermal barrier of the component including exposure to the radiation for the length of time, measuring the temperature obtained, and relating the increase in temperature to the calibration curve in order, from the curve, to extract the level of damage.

Abstract: A device for non-destructive in situ inspection of parts of a turbine engine, the device including a stick carrying at its distal end a pivoting finger carrying at one of its ends a blade for supporting an inspection probe, and at its opposite end a skid for bearing against and/or catching on an element of the engine, the skid being movable in a direction parallel to the longitudinal axis of the finger.