Abstract: A method to increase the thermal stress capability of a porous TBC and layer system. Due to a post treatment step to a pose TBC coating cracks are produced inside the post TBC advantages manner to increase the thermal stress capability of the ceramic coating by only heating the surface of the ceramic coating.

Abstract: A method for predetermining a thickness of a coating which is to be arranged on a substrate is provided. A spray spot is arranged on a surface of the substrate or a test substrate. The volume of the spray spot is determined, and based on the determined volume, the thickness of a layer which is to be applied is worked out. An arrangement for predetermining the thickness of a coating is further provided.

Abstract: An automated method, computer program product and device for determining a thickness of an object at a specific location, such as the determination of a wall thickness of a blade or a vane of a gas turbine. The method includes performing a plurality of ultrasonic measurements around the specific location with an ultrasonic probe of the ultrasonic measurement device, recording and storing the measurement signals, determining at least one apparent thickness of the object for each measurement, sorting the apparent thicknesses in a histogram, and determining the thickness of the object by selecting the most frequently occurring apparent thickness in the histogram.

Abstract: A method to increase the thermal stress capability of a porous TBC and layer system. Due to a post treatment step to a pose TBC coating cracks are produced inside the post TBC advantages manner to increase the thermal stress capability of the ceramic coating by only heating the surface of the ceramic coating.

Abstract: A method for coating a workpiece by using a spraying device is provided. The coating of the workpiece is performed according to at least one coating parameter and at least the following steps are performed during the coating: sensing a locational heat distribution in a working area of a surface of the workpiece; and adjusting the at least one coating parameter in accordance with the sensed heat distribution. A device for coating a workpiece is also provided.

Abstract: A measuring probe head having a housing, which defines a receiving space and at least one coolant fluid supply channel fluidically connected thereto, and at least one sensor which is received, or is capable of being received, in the receiving space, wherein at least one partial region of the housing enclosing the receiving space has a porosity which defines a plurality of coolant fluid passage openings.

Abstract: Provided is a method for determining the external and internal geometry of a component with at least one cavity, wherein a component to be measured is provided with at least one cavity, the external geometry of the component is determined by carrying out a 3D scan, the wall thickness of at least one section of the component is determined using ultrasound, the internal and external component geometry of at least one section of the component in particular is determined using x-ray computer tomography, and the data obtained by means of the 3D scan, the ultrasound wall thickness measurement, and in particular the x-ray computer tomography is combined, wherein the internal geometry of the component in the region of the at least one section measured using ultrasound is reconstructed from the external geometry data of the 3D scan and the data of the ultrasound wall thickness measurement.

Abstract: A turbine blade for a turbomachine, having a blade airfoil with a blade tip region and a sealing region which has an auxetic material and is arranged and designed such that, when transitioning from a rest state to an operating state of the turbine blade, the blade tip region of the turbine blade expands in a first direction perpendicular to a longitudinal axis of the blade airfoil. An auxetic material is used for a turbine blade for sealing a gas path during operation of a turbomachine.

Abstract: A method for predetermining a thickness of a coating which is to be arranged on a substrate is provided. A spray spot is arranged on a surface of the substrate or a test substrate. The volume of the spray spot is determined, and based on the determined volume, the thickness of a layer which is to be applied is worked out. An arrangement for predetermining the thickness of a coating is further provided.

Abstract: The invention relates to a method for coating a workpiece by using a spraying device. The coating of the workpiece is performed according to at least one coating parameter and at least the following steps are performed during the coating: sensing a locational heat distribution in a working area of a surface of the workpiece; and adjusting the at least one coating parameter in accordance with the sensed heat distribution. The invention further relates to a device for coating a workpiece.

Abstract: A monitoring device (14) and a method for monitoring spray coating of a component by a spraying device (1) including a spray nozzle (3) movable along a specific path in relation to a component surface to be coated. The device has: an input interface (15) for inputting geometry data representative of the geometry of the component surface; a path data recording device (17) for time-resolved recording of path data of the spray nozzle (3) in relation to the component surface; a process data recording device (19) for time-resolved recording of process data of the coating process using the spray nozzle (3); a simulation unit (21) connected to the input interface (15) for receiving the data, for simulating application of the spray coating to the component surface on the basis of the data recorded; and a deviation calculation unit (23), connected to the simulation unit (21), for receiving simulation data and calculating a deviation of the simulated coating from the desired coating.

Abstract: A method for additive manufacturing with multiple materials. First (48), second (50), and third (52) adjacent powder layers are delivered onto a working surface (54A) in respective first (73), second (74), and third (75) area shapes of adjacent final materials (30, 44, 45) in a given section plane of a component (20). The first powder may be a structural metal delivered in the sectional shape of an airfoil substrate (30). The second powder may be a bond coat material delivered in a sectional shape of a bond coat (45) on the substrate. The third powder may be a thermal barrier ceramic delivered in a section shape of the thermal barrier coating (44). A particular laser intensity (69A, 69B) is applied to each layer to melt or to sinter the layer. Integrated interfaces (57, 77, 80) may be formed between adjacent layers by gradient material overlap and/or interleaving projections.

Abstract: A method for simulating of the thickness of a coating which is placed onto a substrate surface is disclosed. The thickness is simulated using mass conservation principles. In a preferred embodiment at least one reference spray trial is performed, the correlation of a single spray profile to at least one spray process parameter is determined, the single spray profile is simulated using mass conservation principles to an incoming powder jet stream.

Abstract: A method for generating a motion path for a spray gun for coating a component is disclosed. Path templates for surface segments of the component are defined, the surface is analyzed, a first motion path is generated, a model of the spray profile is simulated, the coating thickness is simulated for the motion path based on the simulated model of the spray profile and the generated first motion path. The simulated coating thickness is compared with tolerances and when the simulated coating thickness does not achieve the tolerances, an adapted motion path is generated. The coating thickness is simulated for the motion path based on the simulated model of the spray profile and the generated adapted motion path. Repeating the comparing, the motion path generation, and the simulation of the coating thickness based on the generated adapted motion path until the simulated coating thickness achieves the tolerances.