Abstract: A method of simultaneously reconstructing and testing a straddle-mount turbine blade hub with the turbine blades in place. The method employs a sector scan ultrasonic phased array mounted on one face of the hub to inspect the opposite face.

Abstract: An apparatus and method for ultrasonic reconstruction and testing of a non-visible turbine rotor blade attachment structure is described. The method of the invention includes positioning transducers at a first location to obtain slot region scan data corresponding to a slot region of the non-visible turbine rotor blade attachment structure, and positioning transducers at a second location to obtain straddle-mount region scan data corresponding to a straddle-mount region of the non-visible turbine rotor blade attachment structure. The shape of the non-visible turbine rotor blade attachment structure is reconstructed from the slot region scan data and the straddle-mount region scan data to form reconstruction data. The reconstruction data is used to select test scan positions for ultrasonic testing. Ultrasonic testing is then performed at the selected test scan positions.

Abstract: An extended flaw in a material is located in two or three dimensions by propagating ultrasonic energy in a predetermined direction in the material and logging receiving transducer positions and ranges at which individual facets on the surface of the flaw produce maximum amplitude ultrasonic returns. The positions of all of the individual facets in the material are calculated from the predetermined direction, receiving transducer positions and the corresponding ranges. The locations of the individual facets outline the extended flaw.