Patent Application
20120033787
This application claims priority to German Patent Application DE102010033761.7 filed Aug. 9, 2010, the entirety of which is incorporated by reference herein.
This invention relates to a method for radiographic inspection of components by X-rays or gamma rays according to the basic principle that the absorption and intensity of the radiation impinging on the radiographic film upon passing the component is changed by material defects.
Radiographic inspection is an imaging method for non-destructive material testing in which a component under inspection is subjected to radiation by use of a suitable radiation source, for example an X-ray tube, and a projected image of the component recorded on radiographic film. Voids, inclusions, segregations, gas cavities, cracks or bonding defects present in the component are made visible due to different radiation absorption and correspondingly changed radiation attenuation, with higher radiation intensity resulting in an increase in density on the radiographic film.
The detectability of material defects is impaired by edge blur, i.e. a penumbra area around the imperfection, and reduced contrast (density difference) which may be caused by scatter of the electromagnetic waves impinging on an irregular component surface. However, an irregular surface structure of the component to be inspected, for example in the form of surface porosity, primarily leads to reduced radiation absorption and correspondingly high radiation intensity. The densities so produced on the radiographic film do however not represent relevant material defects, but rather falsify the inspection result or do not allow precise detection of material defects or safe automatic evaluation of the radiographic films to be made.
In a broad aspect, the present invention provides a method for radiographic inspection of components by which safe detectability of imperfections present in the component material is ensured.
Radiographic inspection of components by use of X-rays or gamma rays is accomplished according to the basic principle that the absorption and intensity of the radiation impinging on the radiographic film upon passing the component is changed by material defects in the component, with the density of the radiographic film being influenced by the intensity of the radiation. The present invention, in essence, provides that an uneven surface topography of the component, which likewise effects changes in radiation intensity, is smoothened or levelled out with a smoothening layer made of a material whose volume-specific radiation absorption corresponds to that of the component material, so that a decrease of radiation absorption or an increase in radiation intensity due to an uneven surface geometry is avoided and density of the radiographic film is only produced by internal material defects. This enables a precise, preferably also automated radiographic inspection to be performed, which is crucial in particular for safety-relevant components.
In a further development of the present invention, the smoothening or levelling layer applied to the component surface is made of a plastically deformable material with metal powder embedded therein.
The maximum metal powder content in the smoothening layer is not higher than required for ensuring adequate deformability of the material in order to produce a smooth, even surface contour.
The smoothening layer is of such a nature that it can be removed or stripped off the component after radiographic inspection.
The method variants according to the present invention enable material defects, such as voids, inclusions, segregations, gas cavities, cracks or bonding defects to be precisely detected both visually and in an automated process.
An embodiment of the present invention is more fully described in light of the accompanying drawing.
In the exemplary embodiment, the component 1, which is shown in highly simplified representation, is made of 18.8 chromium nickel steel and has an uneven surface topography 2 with depressions 3. Two voids 4 are present in the interior of the component 1 to be inspected. The component 1 is subjected to X-ray—indicated by arrows 5. These X-rays penetrate the component and produce on the radiographic film 6a or 6b arranged beneath the component a density 7 corresponding to the radiation intensity I.
As shown in the drawing, the uneven surface topography 2 of the component 1 can be covered by a smoothening layer 8 composed of an easily formable material with metal powder embedded therein. The maximum metal powder content—for example 65 percent—is not higher than required for preventing the powder particles from colliding with each other, enabling the material to be well formed and surface irregularities levelled out, i.e. a smooth, even component surface to be produced. The metal powder is made, for example, of the same material as the component, i.e. 18.8 chromium nickel steel, and of other metal powder additions, so that the smoothening layer 8 has the same X-ray absorption as the base material of component 1.
The lower radiographic film 6b schematically shows the intensity of the X-rays and the corresponding densities on the radiographic film 6b upon penetrating the component 1 without the smoothening layer 8 applied. Due to the uneven surface topography 2, radiation intensity I is very high, also in the area of the depressions 3. The radiographic film 6b therefore shows a multitude of not clearly defined densities 7 which do not allow automatic evaluation of the radiographic film 6b and definite—sharp-edged—identification of the densities 7 caused by the voids 4.
The upper radiographic film 6a shows the intensity of the X-rays 5 and the corresponding densities on the radiographic film 6a upon penetrating the component 1 provided with the smoothening layer 8 described above. Owing to the smoothening layer 8, the X-rays 5 are now absorbed also in the area of the uneven surface topography to the same extent as in the base material of component 1. Increased radiation intensity I with more clearly defined density of the radiographic film 6a is noted only at those locations where the X-rays 5 pass the voids 4 in the wall of component 1. The voids 4 are therefore clearly identifiable also with automatic evaluation of the radiographic film 6a, so that increased safety is ensured, for example, when using safety-relevant components for aerospace applications.
After radiographic inspection the smoothening layer 8 can be stripped off the surface of the component.
| Number | Date | Country | Kind |
|---|---|---|---|
| 10 2010 033 761.7 | Aug 2010 | DE | national |
