Abstract:
A method of imaging a turbine engine test component with a first surface and a second surface that is spaced from the first surface. The turbine engine test component includes a plurality of film holes with inlets formed in the second surface or interior that are fluidly coupled to outlets formed in the first surface or exterior. The method includes flowing airflow through the plurality of film holes of the turbine engine test component, obtaining thermographic data, determining a test dataset, and calculating a performance score.
Abstract:
A method for inspecting a component is presented. The method includes inducing, by an inductive coil, an electrical current flow into the component. Further, the method includes capturing, by an infrared (IR) camera, at least a first set of frames and a second set of frames corresponding to the component, wherein the first set of frames is captured at a first time interval and a second set of frames is captured at a second time interval. Also, the method includes constructing, by a processing unit, a thermal image based on at least the first set of frames and the second set of frames corresponding to the component. Furthermore, the method includes determining presence of a thermal signature in the thermal image, wherein the thermal signature is representative of a defect in the component.
Abstract:
An inspection system includes a thermographic sensor configured to capture thermographic data of a component having holes as a fluid is pulsed toward the holes, and one or more processors configured to temporally process the thermographic data to calculate temporal scores and spatial scores for the corresponding holes. The scores can be used to obtain a reference dataset and a test dataset. A performance score can be assigned to the component based on the difference between the datasets.
Abstract:
An inspection system includes a thermographic sensor configured to capture thermographic data of a component having holes as a fluid is pulsed toward the holes, and one or more processors configured to temporally process the thermographic data to calculate temporal scores and spatial scores for the corresponding holes. The scores can be used to obtain a reference dataset and a test dataset. A performance score can be assigned to the component based on the difference between the datasets.
Abstract:
A method for inspecting a component is presented. The method includes inducing, by an inductive coil, an electrical current flow into the component. Further, the method includes capturing, by an infrared (IR) camera, at least a first set of frames and a second set of frames corresponding to the component, wherein the first set of frames is captured at a first time interval and a second set of frames is captured at a second time interval. Also, the method includes constructing, by a processing unit, a thermal image based on at least the first set of frames and the second set of frames corresponding to the component. Furthermore, the method includes determining presence of a thermal signature in the thermal image, wherein the thermal signature is representative of a defect in the component.
Abstract:
A thermographic nondestructive evaluation system includes a lamp assembly having a lamp. The lamp is configured to be positioned within an internal cavity of a target object and to emit an energy pulse toward an interior surface of the internal cavity. The lamp includes at least one curved portion, the at least one curved portion is curved relative to a longitudinal axis of the lamp, and a first curvature of the curved portion is selected to substantially correspond to a second curvature of the internal cavity.
Abstract:
An additive manufacturing system includes at least one imaging device configured to direct electromagnetic radiation towards a build layer of a component positioned within a powder bed of the additive manufacturing system. The additive manufacturing system also includes at least one detector configured to detect the electromagnetic radiation that reflects from the build layer.
Abstract:
A thermographic nondestructive evaluation system includes a lamp assembly having a lamp. The lamp is configured to be positioned within an internal cavity of a target object and to emit an energy pulse toward an interior surface of the internal cavity. The lamp includes at least one curved portion, the at least one curved portion is curved relative to a longitudinal axis of the lamp, and a first curvature of the curved portion is selected to substantially correspond to a second curvature of the internal cavity.
Abstract:
A method of imaging a turbine engine component with a first surface and a second surface that is spaced from the first surface. The turbine engine component includes a plurality of holes with inlets formed in the second surface or interior that are fluidly coupled to outlets formed in the first surface or exterior. The method includes determining at least one fluid frequency, determining at least one sampling frequency, and pulsing fluid through at least a portion of the interior of turbine engine component while imaging the turbine engine component.
Abstract:
An additive manufacturing system includes at least one imaging device configured to direct electromagnetic radiation towards a build layer of a component positioned within a powder bed of the additive manufacturing system. The additive manufacturing system also includes at least one detector configured to detect the electromagnetic radiation that reflects from the build layer.