Abstract: A measurement system for and method of measuring thicknesses of coatings as applied to objects and a coating system and method for. coating objects, in particular three-dimensional objects, with coatings, in particular thermal barrier coatings (TBCs), and a monitoring system for and method of monitoring a state of a thermal barrier coating (TBC) as applied to an object which is exposed to a high-temperature environment, and a TBC for use with the same.

Abstract: Luminescent material compositions, in particular for use in high-temperature environments, and structures, such as thermal barrier coatings (TBCs), which incorporate the same.

Abstract: A system for and method of determining thermal history of components which are subjected to high-temperature environments, such as in boilers, fuel cells, furnaces, engines and gas turbines, and temperature-monitoring materials and coatings for use in such a system and method.

Abstract: A coating material (20) for coating a machine component (10), especially a gas turbine or a part thereof, comprises a mixture of at least a refractory material and an indicator material having an optical emission (e.g. fluorescence) spectrum which varies in response to a physical parameter of the coated component. In a preferred embodiment, the coating consists of yttrium aluminum garnet (YAG) or yttrium stabilized zirconium. The dopant is preferably a rare earth metal, e.g. Eu, Tb, Dy.

Abstract: A system for and method of determining thermal history of components which are subjected to high-temperature environments, such as in boilers, fuel cells, furnaces, engines and gas turbines, and temperature-monitoring materials and coatings for use in such a system and method.

Abstract: A method for optically detecting hot corrosion of a thermal barrier coating (TBC), comprising: providing a TBC which includes an indicator material which has an optical emission which is altered by corrosion of the coating; irradiating the TBC with an excitation beam of light; receiving an optical emission from the TBC; obtaining a detection signal for the optical emission; and analysing the detection signal to identify one or more predeterminable spectral characteristics and evaluate the amount of corrosion of the TBC. Detection apparatus for optically detecting the corrosion of a thermal barrier coating with the mentioned method, and coating to be inspected by said apparatus and method.

Abstract: A coating material (20) for coating a machine component (10), especially a gas turbine or a part thereof, comprises a mixture of at least a refractory material and an indicator material having an optical emission (e.g. fluorescence) spectrum which varies in response to a physical parameter of the coated component. In a preferred embodiment, the coating consists of yttrium aluminium garnet (YAG) or yttrium stabilised zirconium. The dopant is preferably a rare earth metal, e.g. Eu, Tb, Dy.

Abstract: Luminescent material compositions, in particular for use in high-temperature environments, and structures, such as thermal barrier coatings (TBCs), which incorporate the same.

Abstract: A measurement system for and method of measuring thicknesses of coatings as applied to objects and a coating system and method for coating objects, in particular three-dimensional objects, with coatings, in particular thermal barrier coatings (TBCs), and a monitoring system for and method of monitoring a state of a thermal barrier coating (TBC) as applied to an object which is exposed to a high-temperature environment, and a TBC for use with the same.

Abstract: A coating material (20) for coating a machine component (10), especially a gas turbine or a part thereof, comprises a mixture of at least a refractory material and an indicator material having an optical emission (e.g. fluorescence) spectrum which varies in response to a physical parameter of the coated component. In a preferred embodiment, the coating consists of yttrium aluminium garnet (YAG) or yttrium stabilized zirconium. The dopant is preferably a rare earth metal, e.g. Eu, Tb, Dy.

Abstract: A coating material (20) for coating a machine component (10), especially a gas turbine or a part thereof, comprises a mixture of at least a refractory material and an indicator material having an optical emission (e.g. fluorescence) spectrum which varies in response to a physical parameter of the coated component. In a preferred embodiment, the coating consists of yttrium aluminium garnet (YAG) or yttrium stabilised zirconium. The dopant is preferably a rare earth metal, e.g. Eu, Tb, Dy.