Abstract: Embodiments of the invention relate to a system and method for non-destructively inspecting a component that is at least partially made of a composite material. In one embodiment, the composite component can be a ceramic matrix composite vane or a liner for a turbine engine. Aspects of the invention involve imaging the component using a magnetic resonance imaging (MRI) apparatus. To enhance the image, the component can be infiltrated with at least one contrast media, which can be in liquid or gas form. By imaging the component using the MRI apparatus, internal and/or external defects of the component can be revealed. In addition, internal and/or external features of interest can examined for dimensional accuracy, among other things.

Abstract: Embodiments of the invention relate to a system and method for non-destructively inspecting a component that is at least partially made of a composite material. In one embodiment, the composite component can be a ceramic matrix composite vane or a liner for a turbine engine. Aspects of the invention involve imaging the component using a magnetic resonance imaging (MRI) apparatus. To enhance the image, the component can be infiltrated with at least one contrast media, which can be in liquid or gas form. By imaging the component using the MRI apparatus, internal and/or external defects of the component can be revealed. In addition, internal and/or external features of interest can examined for dimensional accuracy, among other things.

Abstract: A method and apparatus for calibrating an acoustic thermography system 10 and/or enhancing the flaw detection abilities of such a system is provided. The method allows applying a material (e.g., 103) to a specimen 12 undergoing acoustic thermography inspection. The material is thermally responsive to acoustic energy transmitted to the specimen by the acoustic thermography system. In one aspect thereof, a thermal response of the material applied to the specimen when subjected to acoustic energy is processed to determine whether the level of acoustic energy applied by the acoustic thermographic system appropriately meets a desired amount of acoustic energy for inspecting the specimen. In another aspect thereof, the thermal response of the specimen in combination with the applied material may be processed to determine whether certain types of flaws (e.g.

Abstract: The present invention relates to the use of positron annihilation spectroscopy (PAS) as a method for the measurement of material damage in hot gas path components in industrial gas turbines. A method measuring material damage, expended life and remaining life, using PAS, in nickel and cobalt based superalloy turbine components where the damage has been created by engine operational exposure, is provided. The method can also be used to assess damage to metal components in steam turbines, heat exchangers and generators, as well as damage to other metal, ceramic, plastic and composite articles.

Abstract: A method and apparatus for calibrating an acoustic thermography system 10 and/or enhancing the flaw detection abilities of such a system is provided. The method allows applying a material (e.g., 103) to a specimen 12 undergoing acoustic thermography inspection. The material is thermally responsive to acoustic energy transmitted to the specimen by the acoustic thermography system. In one aspect thereof, a thermal response of the material applied to the specimen when subjected to acoustic energy is processed to determine whether the level of acoustic energy applied by the acoustic thermographic system appropriately meets a desired amount of acoustic energy for inspecting the specimen. In another aspect thereof, the thermal response of the specimen in combination with the applied material may be processed to determine whether certain types of flaws (e.g.

Abstract: A thermal imaging system for detecting cracks and defects in a component. An electromagnetic acoustic transducer (EMAT) is coupled to the component, and introduces pulsed sound signals therein. The sound signals cause the defects to heat up. The IR radiation from the heated pulses is detected by a thermal camera. The amplitude of the pulsed signals are substantially constant, and the frequency of the pulsed signal can be changed within each pulse. A control unit is employed to provide timing and control for the operation of the EMAT and the camera.

Abstract: A system with three parts: a testing apparatus, a computer system, and a communications line between the two. The testing apparatus has a device that emits x-rays into the sample, a device to position the sample relative to the x-rays and an electro-optical x-ray detector for detecting diffracted x-rays. The computer system has a computer, a computer program, a storage device, a database, and monitor or other means of announcing the results of a test. The computer program directs the computer to accept data from the sample testing system concerning the relationships of the devices, the x-rays, and diffracted x-rays. The computer program also directs the computer to compare this data with a database of previously determined relationships and possible diffraction patterns stored in the storage device. Based on the comparison, the computer program directs the computer to announce the results of the comparison via the monitor or other means, thereby revealing the crystallographic grain structures of the sample.

Abstract: A sensing device for protecting a sensor from environmental conditions present in a turbine is provided. The sensing device comprises a heat pipe exposed to the environmental conditions for protecting the sensor from these conditions. The sensing device further comprises a sensor located in a center channel of the heat pipe and a working fluid located in an annulus of the heat pipe to aid in regulating heat along the length of the heat pipe. In alternate embodiments, the sensing device further comprises power wires extending from a power source outside the turbine to the sensor for supplying power to the sensor, and signal wires extending from the sensor to a data acquisition system outside the turbine for transmitting readings from the sensor to the data acquisition system.