发明名称 In situ combustion turbine engine airfoil inspection
摘要 A system ( 10 ) for imaging a combustion turbine engine airfoil includes a camera ( 12 ) and a positioner ( 24 ). The positioner may be controlled to dispose the camera within an inner turbine casing of the engine at a first position for acquiring a first image. The camera may then be moved to a second position for acquiring a second image. A storage device ( 30 ) stores the first and second images, and a processor ( 32 ) accesses the storage device to generate a composite image from the first and second images. For use when the airfoil is rotating, the system may also include a sensor ( 40 ) for generating a position signal ( 41 ) responsive to a detected angular position of an airfoil. The system may further include a trigger device ( 42 ), responsive to the position signal, for triggering the camera to acquire an image when the airfoil is proximate the camera.
申请公布号 US2005199832(A1) 申请公布日期 2005.09.15
申请号 US20040797451 申请日期 2004.03.10
申请人 SIEMENS WESTINGHOUSE POWER CORPORATION 发明人 TWERDOCHLIB MICHAEL
分类号 G01N21/86;G01V8/00;(IPC1-7):G01V8/00 主分类号 G01N21/86
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