SHEAROGRAPHY AND INTERFEROMETRY SENSOR WITH MULTIDIRECTIONAL DYNAMIC PHASE SHIFTING AND METHOD OF INSPECTION AND MEASUREMENT OF VIBRATION MODES

Abstract

The present invention addresses to a multidirectional dynamic phase shifting interferometry (DPSI) shearography and interferometry sensor. The present invention uses a configuration with three fixed prisms, or a single fixed three-facet optical prism constructed so as to achieve the same effect as three prisms and thus simultaneously obtain three images with phase shifting. The present invention also encompasses a method of inspection and measurement of vibration modes using said sensor.

Claims

1- A SHEAROGRAPHY AND INTERFEROMETRY SENSOR WITH MULTIDIRECTIONAL DYNAMIC PHASE SHIFTING, comprising a multidirectional measurement head interconnected, on one side, to a charging or excitation module, and, on the other side, to a lighting laser, which are supported by a fixing structure.

2- THE SHEAROGRAPHY AND INTERFEROMETRY SENSOR WITH MULTIDIRECTIONAL DYNAMIC PHASE SHIFTING according to claim 1, wherein the multidirectional measurement head comprises a digital video camera, a digital camera image sensor, an internal lens, an aperture mask, an optical prism and an objective lens.

3- THE SHEAROGRAPHY AND INTERFEROMETRY SENSOR WITH MULTIDIRECTIONAL DYNAMIC PHASE SHIFTING, according to claim 2, wherein the digital camera image sensor is of the CCD or CMOS type.

4- THE SHEAROGRAPHY AND INTERFEROMETRY SENSOR WITH MULTIDIRECTIONAL DYNAMIC PHASE SHIFTING according to claim 2, wherein the sensor is a three-facet optical prism.

5- THE SHEAROGRAPHY AND INTERFEROMETRY SENSOR WITH MULTIDIRECTIONAL DYNAMIC PHASE SHIFTING according to claim 2, further comprising three wedge-shaped optical prisms (W.sub.1-3).

6- THE SHEAROGRAPHY AND INTERFEROMETRY SENSOR WITH MULTIDIRECTIONAL DYNAMIC PHASE SHIFTING according to claim 1, comprising optical components for simultaneous measurement of shearography and DPSI, wherein said optical components are a semi-mirror or beam splitter and a first surface mirror disposed at 45°.

7- A METHOD OF INSPECTION AND MEASUREMENT OF VIBRATION MODES, using the shearography and interferometry sensor with multidirectional dynamic phase shifting as defined in claims 1 to 6, comprising: a) Positioning of said shearography and interferometry sensor with multidirectional dynamic phase shifting in front of the inspection area; b) Acquisition of the image of the reference state; c) Application of the load for excitation of the repair; d) Acquisition of the image of the structure in the deformed state (Δϕ); e) Processing of the acquired images with the presentation of the final images with the fringe maps in the three sensitivity directions for the identification of defects.

Description

BRIEF DESCRIPTION OF DRAWINGS

[0014] The present invention will be described in more detail below, with reference to the attached figures, which, in a schematic way and not limiting the inventive scope, represent examples of its embodiment. In the drawings, there are:

[0015] FIG. 1 illustrates a diagram of the triple displacement formation using three wedge-shaped prisms;

[0016] FIG. 2 illustrates a representation of the displacement caused by the arrangement of three wedge-shaped prisms;

[0017] FIG. 3 illustrates an optical arrangement for triple shearography with three apertures;

[0018] FIG. 4 illustrates a diagram of the different combinations of apertures, a speckle simulation with carrier fringes, an equivalent spectrum by fast Fourier transform and equivalent laterally displaced images;

[0019] FIG. 5 illustrates steps to extract the different phase maps for each displacement component. Acquired image and its two-dimensional frequency spectrum by fast Fourier transform. Extraction of the main components in the Fourier plane by applying an elliptical band pass filter. Resulting phase maps of each component. Enlarged view of a region of the phase map, showing the orientation of the carrier fringes;

[0020] FIG. 6 illustrates a simulation of the phase difference maps for triple shearography;

[0021] FIG. 7 illustrates a configuration for simultaneous measurement of shearography and DSPI;

[0022] FIG. 8 illustrates a simulation of the simultaneous results of shearography and DSPI;

[0023] FIG. 9 illustrates a general configuration of a shearography system for non-destructive inspections in composite material repair;

[0024] FIG. 10 illustrates internal components of the multidirectional shearography head;

[0025] FIG. 11 illustrates the addition of optical components for simultaneous measurement of Shearography and DPSI;

[0026] FIG. 12 illustrates the simultaneous measurement for a circular specimen with mechanical loading applied by a micrometric screw supported at its posterior central point. Dimensions of the aluminum circular plate: 2 mm of thickness and 150 mm of diameter;

[0027] FIG. 13 illustrates the simultaneous measurement with a flat aluminum specimen coated in composite material and excited with thermal loading. The fringe concentrations show the positions of the internal defects;

[0028] FIG. 14 illustrates the simultaneous measurement of a gutter-shaped specimen with composite coating and thermal loading. The central fringes show the position of the defect repaired by the coating;

[0029] FIG. 15 illustrates an experimental configuration for simultaneous measurement of DSPI-Shearography;

[0030] FIG. 16 illustrates phase maps resulting from the simultaneous measurement of DSPI-Shearography;

[0031] FIG. 17 illustrates a specimen for testing the visualization of vibration modes;

[0032] FIG. 18 illustrates the experimental configuration to visualize the vibration modes;

[0033] FIG. 19 illustrates images of circular membrane vibration modes obtained with the proposed configuration in DSPI. Increasing frequency from left to right and from top to bottom;

[0034] FIG. 20 illustrates images of circular membrane vibration modes obtained with the shearography configuration and lateral displacement in y. Increasing frequency from left to right and from top to bottom.

DETAILED DESCRIPTION OF THE INVENTION

[0035] The present invention will be described in detail below with reference to the above-mentioned Figures, which in no way signify or represent limitations that may be imposed on the inventive scope as claimed herein. In this sense, and to facilitate the understanding of the constituent elements of the invention, the following reference list is presented: [0036] 1—Reference point [0037] 2—Bulkhead [0038] 3—Camera sensor [0039] 4—Triple lateral displacement [0040] L1—Lens [0041] W1-3—Wedge-shaped prisms [0042] 5—Reference image [0043] 6—Triple displacement image [0044] Z—Distance from aperture to camera sensor 3 [0045] 8—Combination of apertures [0046] 9—Simulation of carrier fringes [0047] 10—Fast Fourier Transform [0048] 11—Equivalent lateral displacement [0049] 12-14—Combinations of two apertures [0050] 15—Combination of three apertures [0051] *—Opposition in relation to origin [0052] A.sub.1-3—Apertures [0053] C.sub.x—Displacement on the x axis [0054] A.sub.x—Arrangement on the x axis [0055] C.sub.y—Displacement on the y axis [0056] A.sub.y—Arrangement on the y axis [0057] C.sub.xy—Displacement at −45° from the x-axis direction [0058] A.sub.xy—Arrangement on the straight line at −45° from the [0059] x-axis direction [0060] A—Arrangement at origin [0061] 16—Filtered Fast Fourier Transforms [0062] 17—Phase maps [0063] 18—Orientation of the lateral displacement [0064] 19—Reference beam [0065] 20—Mirror [0066] 22—Displaced images [0067] S.sub.y—Carrier fringes for the shearography components on the y-axis [0068] H.sub.x—Carrier fringes for the DSPI components on the y-axis [0069] H.sub.xy—Carrier fringes for DSPI components at −45° from the x-axis direction [0070] Δϕ—Phase map resulting from the difference between the deformed map (acquired after loading) and the reference map [0071] 23—Multidirectional measurement head [0072] 24—Charging or excitation module [0073] 25—Lighting laser [0074] 26—Fixing structure [0075] 27—Repair in composite material with internal defect [0076] 28—Metal Pipe with through-hole [0077] f1—Focal length 1 [0078] f2—Focal length 2 [0079] 29—Video camera [0080] 30—CCD or CMOS Image Sensor [0081] 31—Internal lens [0082] 32—Mask of apertures [0083] 33—Three-facet optical prism [0084] 34—Objective lens [0085] 35—Semi-mirror or Beam splitter [0086] 36—First surface mirror [0087] 37—Specimen [0088] 38—DSPI-Shearography multidirectional head [0089] 39—Original phase difference maps [0090] 40—Phase difference maps after applying a sine/cosine low pass filter [0091] 41—Phase difference maps after processing for phase jump removal [0092] 42—Loudspeaker [0093] 43—Circular membrane [0094] 44—Beam splitter [0095] 45—Acquired image and its two-dimensional frequency spectrum by Fast Fourier Transform [0096] 46—Extraction of the main components in the Fourier plane by applying an elliptical band pass filter [0097] 47—Resulting phase maps of each component [0098] 48—Enlarged view of a region of the phase map, showing the orientation of the carrier fringes [0099] 49—Fast Fourier Transform, DSPI-Shearography [0100] w—Out-of-plane displacement component [0101] s—Deformation field

[0102] The use of the present invention is to perform instantaneous measurements of shearography or speckle interferometry (DSPI) in multiple directions of sensitivity.

[0103] Multiple directions of shearography sensitivity (4) can be captured simultaneously using a single image (1) with the addition of a new optical component. A third wedge-shaped prism (W3) was included in the configuration to generate a third laterally displaced image, as shown in FIG. 1. FIG. 2, in turn, illustrates the image of a triangle (5) when captured by the camera sensor (3) in this configuration. The main difficulty of this configuration is the data complexity generated by the interference of three displaced images (6), causing greater computational effort to separate each displacement component in the Fourier spectrum.

[0104] In order to enable the separation of the three displacement components in the Fourier spectrum, three apertures are included in the optical configuration (7), as shown in FIG. 3. The three apertures (7) function as three pairs of apertures, and each pair generates a set of carrier fringes with three different orientations, allowing to isolate each component in the Fourier spectrum.

[0105] FIG. 4 shows the different arrangements (13-15) of aperture (8), the resulting Fourier spectrum (10) and the respective displacement images (11) observed by the camera sensor (3).

[0106] According to the provisions (8) presented in FIG. 4, the arrangement (A.sub.2,3 8;12) generates a set of carrier fringes (9;12) in the direction of the y axis, (A.sub.1,2 8;13) generates a set of carrier fringes (9;13) in the x-axis direction, and (A.sub.1,3 8;14) generates an oblique set of carrier fringes (9;14) at −45° of the x-axis direction. Therefore, each pair of apertures produces a set of carrier fringes perpendicular to the line joining their centers (9). The carrier fringe contains the interference generated by the double image (11)—a laterally displaced image, produced by a pair of prisms W.

[0107] Each component C in the Fourier spectrum (10) corresponds to a single lateral displacement shift orientation. C.sub.x indicates a lateral displacement in the x-axis direction (10;13). C.sub.xy denotes a transverse displacement at −45° (10;14) and C.sub.xy a displacement at −135° (10;12). In this way, with only a single reference image (5), it is possible to obtain information from the three phase maps (17) simultaneously, in different displacement directions. This fact leads to an increase in speed and consequently a gain in productivity of the inspection process by shearography. FIG. 5 shows the image processing steps (45-48) to retrieve the reference phase map (17) for each displacement component.

[0108] The same process is repeated for the images of the structure in the deformed state, produced by the application of a load. Therefore, from the difference between the reference image and the one after a deformation, it is possible to obtain, from a single shearography measurement, the phase difference maps referring to three different displacement directions (18). The resulting maps are shown in FIG. 6.

[0109] With some adaptations to the configuration of multiple apertures presented above, it is possible to have an alternative configuration that allows to obtain, in a simultaneous way, results of two interferometric techniques: shearography and DSPI (Digital Speckle Pattern Interferometry).

[0110] Configuration Adaptation with Multiple Apertures for Simultaneous Measurement DSPI-Shearography:

[0111] As shown in FIG. 7, if the third aperture contains a coherent reference beam (19) it is possible to obtain, always from a single acquisition for each loading state, two simultaneous results (49): one of DSPI (Digital Speckle Pattern Interferometry) that results in a displacement field, and a shearography field that results in the fields of the derivatives of displacements (or deformation gradient), given a lateral displacement direction.

[0112] FIG. 8 shows a simulation of the result with the proposed configuration. The halos identified by the letter H in the fast Fourier transform image (49) represent the spectrum of the carrier fringes for the DSPI components and the S halos represent the carrier fringes for the shearographic components.

[0113] With this new optical arrangement, it is possible to obtain, simultaneously, the “out-of-plane” displacement field (DSPI) and the deformation gradient (shearography) for the analyzed surface. Obtaining both results facilitates the extraction of mechanical parameters from the structure and complements the mechanical analysis.

[0114] The optical configurations detailed above are applied within the measurement heads (23) of non-destructive inspection systems.

[0115] The multidirectional head for multidirectional shearography/DPSI measurements is simply coupled to the computer by means of the specific video camera interface (29) used in the equipment, such as a USB or GigE interface. The acquisition of images is performed by means of this interface.

[0116] The inspection system is basically composed of the following components: a multidirectional measurement head (23) interconnected, on one side, to a charging or excitation module (24), and, on the other side, to a lighting laser (25), which are supported by a fixing structure (26). In addition to showing the basic components of a shearography system, FIG. 9 also illustrates the inspection of a defective composite coating (27) applied to metallic piping (28). This piping may also contain defects in its metal wall, such as loss of thickness or through-hole (28).

[0117] The inspection procedure using multidirectional shearography for the non-destructive analysis of composite repair can be divided into the following steps: [0118] a) Positioning the shearography system in front of the inspection area; [0119] b) Acquisition of the image of the reference state; [0120] c) Application of the load for excitation of the repair; [0121] d) Acquisition of the image of the structure in the deformed state; [0122] e) Processing (subtraction) of the acquired images with presentation of the final images with the Fringe Maps (also called Phase Difference Maps) in the three directions of sensitivity for the identification of defects by the inspector.

[0123] Since the present invention is aimed at multidirectional shearography, only the operation of the multidirectional head will be detailed below.

[0124] The multidirectional head, as illustrated in FIG. 10, comprises the following components: a digital video camera (29), a digital camera image sensor (30), an internal lens (31), an aperture mask (32), a prism optic (33) and an objective lens (34).

[0125] The surface of the inspected structure reflects laser light (25) towards the multidirectional inspection head. Laser light reflected from the composite surface enters the multidirectional head through the objective lens (34), and is projected onto the image sensor (30) after passing through the internal components of the head. The internal components (31-33) are responsible for the formation of the double image and the carrier fringes in the three preferred measurement directions. The processing to obtain the shearography results is done as previously described.

[0126] For simultaneous measurement of DPSI and shearography, the optical arrangement of the system is modified with the insertion of a semi-mirror (beam splitter) (35) and a first surface mirror (36) arranged at 45° to direct the reference beam to the image sensor (30), as shown in FIG. 11. The processing to obtain the shearography results is done as previously described.

[0127] Several measurements using the configuration according to the present invention were performed for different specimens, and their results are shown in the figures described below. The following figures also show the experimental configuration, as well as the three simultaneous shearography/DPSI results obtained before and after the application of a low-pass filter.

[0128] The results shown in FIG. 12-14 demonstrate the feasibility of instantaneous shearography measurement in three different lateral displacement directions (4), by means of the multiple aperture principle (7) and the three-facet optical prism W.

[0129] DSPI-Shearography Simultaneous Measurement:

[0130] The measurement of the displacement component outside the plane w by Speckle Interferometry (DSPI) and, simultaneously, the measurement of the deformation field s by shearography, was validated by means of the configuration presented in FIG. 7, whose experimental configuration is shown in FIG. 15. The specimen used in the validation was the same as shown in FIG. 12. The mechanical loading is performed by means of a micrometric screw, positioned at the central point behind the plate to provide a controlled deformation. The phase difference maps resulting from the measurement are shown in FIG. 16.

[0131] Measurement of Vibration Modes:

[0132] Additionally, measurements were made of the vibration modes of a latex membrane, painted with white matte paint, glued to the end of an acrylic tube. Vibration loading was carried out by means of a loudspeaker glued to the other end of the tube. The specimen is shown in FIG. 17 and the experimental configuration in FIG. 18. The excitation signal was generated by means of a function generator connected to the loudspeaker. In the experimental configuration, the DSPI-Shearography configuration was used, where it is possible to directly measure the out-of-plane displacement component.

[0133] The images obtained were processed in the Fourier plane and the results for each vibration mode, after applying a low pass filter to reduce speckle noise, are shown in FIG. 19 and FIG. 20.