초록 ▼

A non-destructive method of detecting and measuring machining induced surface defects on gas turbine engine components is provided. In an exemplary embodiment, the method includes positioning an evanescent microwave microscope probe adjacent a turbine component surface, and scanning the turbine comp

A non-destructive method of detecting and measuring machining induced surface defects on gas turbine engine components is provided. In an exemplary embodiment, the method includes positioning an evanescent microwave microscope probe adjacent a turbine component surface, and scanning the turbine component surface by moving at least one of the evanescent microwave microscope probe and the component surface in an x-y plane while maintaining a predetermined distance between the probe and the component surface constant.

대표청구항 ▼

What is claimed is: 1. A non-destructive method of detecting and measuring machining induced surface and microstructural defects on gas turbine engine components, said method comprising: positioning an evanescent microwave microscope probe adjacent a surface of a gas turbine engine component; and d

What is claimed is: 1. A non-destructive method of detecting and measuring machining induced surface and microstructural defects on gas turbine engine components, said method comprising: positioning an evanescent microwave microscope probe adjacent a surface of a gas turbine engine component; and detecting and measuring machine-induced surface and microstructural defects by scanning the turbine component surface by moving at least one of the evanescent microwave microscope probe and the component surface in an x-y plane while maintaining a predetermined distance between the probe and the component surface constant; and calculating a thickness of a surface damaged layer of the component surface at each scan point. 2. A method in accordance with claim 1 wherein the evanescent microwave microscope probe comprises a metal probe tip having an end sharpened to a point and further comprises a conductive surface of at least one of silver, gold, platinum, palladium and alloys thereof, said positioning an evanescent microwave microscope probe adjacent a turbine component surface comprises positioning the sharpened probe tip a predetermined distance from the turbine component surface. 3. A method in accordance with claim 2 wherein a detector is coupled to the evanescent microwave microscope probe, said method further comprises detecting reflected microwave radiation with the detector coupled to the evanescent microwave microscope probe. 4. A method in accordance with claim 3 wherein the detector is coupled to a computer, said method further comprises sending detected reflected microwave radiation data to the computer. 5. A method in accordance with claim 4 further comprises generating graphical plots from detected reflected microwave radiation data showing the morphology of the component surface. 6. A non-destructive method of detecting and measuring machining induced surface and microstructural defects on gas turbine engine components, said method comprising: positioning an evanescent microwave microscope probe adjacent a surface of a gas turbine engine component; and detecting and measuring machine-induced surface and microstructural defects by scanning the turbine component by moving at least one of the evanescent microwave microscope probe and the component surface in relation to one another in an x-y plane while maintaining a distance between the probe and the turbine component surface constant; wherein the evanescent microwave microscope probe comprises a metal probe tip having an end sharpened to a point and further comprises a conductive surface of at least one of silver, gold, platinum, palladium and alloys thereof; and calculating a thickness of a surface damaged layer of the component surface at each scan point. 7. A method in accordance with claim 6 wherein the evanescent microwave microscope probe is coupled to a detector, said method further comprises detecting reflected microwave radiation with the detector coupled to the evanescent microwave microscope probe. 8. A method in accordance with claim 7 wherein the detector is coupled to a computer, said method further comprises sending detected reflected microwave radiation data to the computer. 9. A method in accordance with claim 8 further comprising generating graphical plots from detected reflected microwave radiation data showing the morphology of the turbine component surface. 10. A non-destructive method of detecting and measuring machining induced surface and microstructural defects on gas turbine engine components, said method comprising: positioning an evanescent microwave microscope probe adjacent a surface of a gas turbine engine component; scanning the turbine component by moving at least one of the evanescent microwave microscope probe and the component surface in relation to one another in an x-y plane while maintaining a distance between the probe and the turbine component surface constant; detecting reflected microwave radiation with a detector coupled to the evanescent microwave microscope probe; wherein the evanescent microwave microscope probe comprises a metal probe tip having an end sharpened to a point and further comprises a conductive surface of at least one of silver, gold, platinum, palladium and alloys thereof; and detecting and measuring machine-induced surface and microstructural defects using the detector; and calculating a thickness of a surface damaged layer of the component surface at each scan point. 11. A method in accordance with claim 10 wherein the evanescent microwave microscope system comprises a computer coupled to the detector, said method further comprises sending detected reflected microwave radiation data to the computer. 12. A method in accordance with claim 11 further comprising generating graphical plots from detected reflected microwave radiation data showing the morphology of the turbine component surface.