Abstract: An apparatus and a method for automatic inspection of through-holes of a component is provided. The proposed apparatus includes an imaging module, an image processing module and an analysis module. The imaging module generates a thermographic image of the component by passing a medium through the through-holes and capturing infra-red radiation emitted from the component while the medium is flowing through the through-holes. The image processing module fits the thermographic image on a digital image obtained from geometrical data of the component. The image processing module is further masks the fitted thermographic image using a digital image mask to extract regions corresponding to through-holes in the thermographic image. The digital image mask is computed based on a determination of positions of through-holes on the digital image. The analysis module evaluates the masked thermographic image to determine an irregularity or blockage in one or more of the through-holes.

Abstract: A testing system for examining the coating and open cooling-air holes of turbine blades includes a positioning device for an infrared camera with two degrees of freedom, a rotating-pivoting device for positioning the turbine blade, and a rotatable air duct arranged on the rotating-pivoting device. The rotatable air duct is configured for introducing into the turbine blade air at a temperature higher or lower in comparison with the turbine blade.

Abstract: By combined flow of gas in the hollow component with outlet holes in a body of the component and thermographic measurement of heated air exiting the component through the outlet holes, the component can be examined. The component is examined in an apparatus in respect of its cooling air consumption and selected desired cross sections of cooling-air openings. A process is to supply gas to a gas calming chamber, convey the calmed gas into the component, and thermographically measure the gas exiting the outlet holes.

Abstract: A gravity center neutral eccentric is provided. The gravity-center-neutral eccentric includes an axis of rotation and an eccentric region, wherein the center of mass of the eccentric lies on the axis of rotation. In another embodiment, a center of mass of the eccentric region also lies on the axis of rotation. A measurement device including a gravity center neutral eccentric is also provided.

Abstract: Method for object marking using a three-dimensional surface inspection system using two-dimensional recordings and method by simple recording of two-dimensional images of a component and comparing the images with a known three-dimensional model for enabling the three-dimensional real structure of a component to be captured using best fit. Photographing measuring points in a measuring point pattern and orienting the component with reference to markers at the points enables orienting the two-dimensional images with the three-dimensional model.

Abstract: The three-dimensional real structure of a component can be captured by means of best fit by simply recording two-dimensional images and comparing a known three-dimensional model. A component is placed on a measurement stage having reference marks and is photographed several times in two-dimensions. The photo recordings are compared with a three-dimensional model of the component. A three-dimensional model is produced using best fit of the two-dimensional recordings and the stored model.

Abstract: A self-centering clamping device for a blade includes a mount having a root reception orifice which has a contour adapted to a root of the blade. The root reception orifice extends in the vertical direction and has a vertically running groove for receiving at least part of the root of the blade. A rotatable roller is arranged in a lower region of the root reception orifice and forms a stop for the root of the blade, a contact region of the roller for the root lying in an angular range larger than 0° and smaller than 90°, and the angular range being oriented upward and into the root reception orifice.

Abstract: An apparatus and a method for automatic inspection of through-holes of a component is provided. The proposed apparatus includes an imaging module, an image processing module and an analysis module. The imaging module generates a thermographic image of the component by passing a medium through the through-holes and capturing infra-red radiation emitted from the component while the medium is flowing through the through-holes. The image processing module fits the thermographic image on a digital image obtained from geometrical data of the component. The image processing module is further masks the fitted thermographic image using a digital image mask to extract regions corresponding to through-holes in the thermographic image. The digital image mask is computed based on a determination of positions of through-holes on the digital image. The analysis module evaluates the masked thermographic image to determine an irregularity or blockage in one or more of the through-holes.

Abstract: A measuring device for a moment weighing system is provided. The measuring device includes a base plate with a plurality of fixing openings, a receiving plate, arranged rotatably on the base plate, including a plurality of receiving openings and a plurality of fixing openings, a measurement receptacle, arranged on the receiving plate for a measurement object, with the measurement receptacle engaging in part of the receiving openings, and a plurality of fixing pins which fix the measurement receptacle in a measurement position by way of engagement in part of the fixing openings in the base plate and receiving plate.

Abstract: A testing system for examining the coating and open cooling-air holes of turbine blades includes a positioning device for an infrared camera with two degrees of freedom, a rotating-pivoting device for positioning the turbine blade, and a rotatable air duct arranged on the rotating-pivoting device. The rotatable air duct is configured for introducing into the turbine blade air at a temperature higher or lower in comparison with the turbine blade.

Abstract: A gravity center neutral eccentric is provided. The gravity-center-neutral eccentric includes an axis of rotation and an eccentric region, wherein the center of mass of the eccentric lies on the axis of rotation. In another embodiment, a center of mass of the eccentric region also lies on the axis of rotation. A measurement device including a gravity center neutral eccentric is also provided.

Abstract: A measuring device for a moment weighing system is provided. The measuring device includes a base plate with a plurality of fixing openings, a receiving plate, arranged rotatably on the base plate, including a plurality of receiving openings and a plurality of fixing openings, a measurement receptacle, arranged on the receiving plate for a measurement object, with the measurement receptacle engaging in part of the receiving openings, and a plurality of fixing pins which fix the measurement receptacle in a measurement position by way of engagement in part of the fixing openings in the base plate and receiving plate.