Abstract:
A flash thermography device (40) for generating an infrared image of a turbine component located inside a turbine (10). The device includes a flash enclosure (46) having an aperture (48). A flash source (50) is located in the aperture wherein the flash source generates a light pulse that heats the turbine component. The device also includes an infrared sensor (42) for detecting thermal energy radiated by the turbine component wherein the radiated thermal energy is transmitted through the aperture to the infrared sensor to enable generation of an infrared image of the turbine component.
Abstract:
A camera scope inspection system with a flexible, tether mounted camera head that is maneuverable in confined internal cavities of power generation machinery. A camera head position sensing system inferentially determines the three dimension (3D) position of the camera head within the inspected machinery. Camera head position data are correlated with camera image data by a controller. In this manner correlated internal inspection image data and corresponding position data are available for future analysis and image tracking.
Abstract:
A system for automated condition assessment of a turbine component is provided. The system includes a partially enclosed photobox and a controller. The partially enclosed photobox includes a configurable rotational table adapted to carry the turbine component, at least one wall perpendicular to and abutting a horizontal platform upon which the rotational table is carried. The photobox also includes a plurality of cameras configured to be automatically positioned at locations surrounding the turbine component and capture images of the turbine component. The controller communicates with each of the cameras to respectively control the positioning of each camera in order to capture a desired view of the turbine component. At least one of the cameras is an infrared camera configured to perform flash thermography capturing a thermographic image of a portion of the turbine component. The thermographic image is used to assess the condition of the turbine component.
Abstract:
A wearable device (102) is provided that is configured to carry out an inspection of a gas turbine or other type of system (148). The device may include a processor (104), a data store (110), at least one output device (112), and at least one input device (118). The processor in the wearable device is responsive to inputs through the at least one input device and set of tasks (142) stored in the data store corresponding to an inspection (140) of the system to provide outputs (220, 234) through the at least one output device that prompt a user to gather data (150) associated with the system being inspected using the wearable device while the wearable device is mounted to the user without the user holding the wearable device with the hand of the user. Also, the processor in the wearable device is configured to generate and output an inspection report (152) responsive to the set of tasks and the data gathered using the wearable device.
Abstract:
Turbine engine rotor (22) corresponding thru-bolts (26) and disc cavities (24) are inspected with a camera inspection system (40,60) that includes one or both of a thru-bolt male threads inspection apparatus and a rotor disc cavity inspection apparatus. The thru- bolts threads inspection apparatus engages the male threads and advances along the bolt threads pattern, selectively capturing camera images at desired spatial positions along the threads pattern. The plural camera (44, 66) threads images are desirably combined to form a composite image of a desired portion of or the entire thru-bolt male threads profiles, which aids their inspection evaluation and provides an archived composite image of the profiles.
Abstract:
Turbine engine rotor (24) corresponding thru-bolts (26) and disc cavities (30) are inspected with a camera inspection system that includes one or both of a thru-bolt male threads inspection apparatus (50) and a rotor disc cavity inspection apparatus (40). The disc cavity inspection scope apparatus is insertable in one or more of the desired rotor disc cavities (30) and orients an attached inspection camera field of view generally transverse to the circumferential wall in the rotor disc that defines the cavity. Preferably inspection scope apparatus insertion into the disc cavities is performed with a motion control system that monitors spatial position of the camera field of view relative to the recess circumferential wall. The plural camera cavity circumferential wall images are desirably combined to form a composite image of a desired portion of or the entire disc cavity circumferential surface, which aids their inspection evaluation and provides an archived composite image of the surface.