EP3630409A1 - Non-destructive evaluation of additive manufacturing components - Google Patents
Non-destructive evaluation of additive manufacturing componentsInfo
- Publication number
- EP3630409A1 EP3630409A1 EP18806671.6A EP18806671A EP3630409A1 EP 3630409 A1 EP3630409 A1 EP 3630409A1 EP 18806671 A EP18806671 A EP 18806671A EP 3630409 A1 EP3630409 A1 EP 3630409A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- sensor array
- evaluated
- coil
- additive manufacturing
- component
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K31/00—Processes relevant to this subclass, specially adapted for particular articles or purposes, but not covered by only one of the preceding main groups
- B23K31/12—Processes relevant to this subclass, specially adapted for particular articles or purposes, but not covered by only one of the preceding main groups relating to investigating the properties, e.g. the weldability, of materials
- B23K31/125—Weld quality monitoring
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K26/00—Working by laser beam, e.g. welding, cutting or boring
- B23K26/34—Laser welding for purposes other than joining
- B23K26/342—Build-up welding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B33—ADDITIVE MANUFACTURING TECHNOLOGY
- B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
- B33Y50/00—Data acquisition or data processing for additive manufacturing
- B33Y50/02—Data acquisition or data processing for additive manufacturing for controlling or regulating additive manufacturing processes
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N27/00—Investigating or analysing materials by the use of electric, electrochemical, or magnetic means
- G01N27/72—Investigating or analysing materials by the use of electric, electrochemical, or magnetic means by investigating magnetic variables
- G01N27/82—Investigating or analysing materials by the use of electric, electrochemical, or magnetic means by investigating magnetic variables for investigating the presence of flaws
- G01N27/90—Investigating or analysing materials by the use of electric, electrochemical, or magnetic means by investigating magnetic variables for investigating the presence of flaws using eddy currents
- G01N27/904—Investigating or analysing materials by the use of electric, electrochemical, or magnetic means by investigating magnetic variables for investigating the presence of flaws using eddy currents with two or more sensors
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R33/00—Arrangements or instruments for measuring magnetic variables
- G01R33/02—Measuring direction or magnitude of magnetic fields or magnetic flux
- G01R33/04—Measuring direction or magnitude of magnetic fields or magnetic flux using the flux-gate principle
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N27/00—Investigating or analysing materials by the use of electric, electrochemical, or magnetic means
- G01N27/72—Investigating or analysing materials by the use of electric, electrochemical, or magnetic means by investigating magnetic variables
- G01N27/82—Investigating or analysing materials by the use of electric, electrochemical, or magnetic means by investigating magnetic variables for investigating the presence of flaws
- G01N27/90—Investigating or analysing materials by the use of electric, electrochemical, or magnetic means by investigating magnetic variables for investigating the presence of flaws using eddy currents
- G01N27/9013—Arrangements for scanning
Definitions
- the present invention relates in general to non-destructive evaluation (NDE) techniques for use in manufacturing and more specifically to a non-destructive evaluation of components made by additive manufacturing processes using an array eddy current system and method.
- Additive Manufacturing refers to a process by which digital three-dimensional design data is used to build up a component from sequentially deposited layers of material. As opposed to milling a component from solid block of material, additive manufacturing builds up components layer by layer using materials which are available in fine powder or other forms (e.g. solid wire). A range of different metals, plastics and composite materials may be used for this purpose. The strengths of additive manufacturing often lie in those areas where conventional manufacturing has reached its limitations.
- Additive manufacturing allows for the fabrication of highly complex structures which can still be extremely light and stable. This process also provides a high degree of design freedom, the optimization and integration of functional features, the manufacture of small batch sizes at reasonable unit costs, and a high degree of product customization even in serial production.
- a powder based additive manufacturing process typically starts by applying a thin layer of the powdered material to a building platform. A powerful laser beam then fuses the powder at exactly the points defined by the computer- generated component design data. The platform is then lowered, and another layer of powder is applied. The material is again fused to bond with the layer below at the predefined points.
- components can be manufactured using stereolithography, laser sintering, laser melting, electron beam melting, direct energy deposition or other technologies commonly referred as 3D printing.
- Various non-destructive evaluation techniques may be used as a single modality or in combination for examining critical additive manufacturing components after the fabrication thereof.
- post additive manufacturing examination may be very challenging, if even possible, for certain components having complex shapes, where the full benefits of the additive manufacturing process are realized.
- a possible approach to addressing this issue would be to conduct very comprehensive monitoring and examination of the additive manufacturing components during fabrication, ideally layer-by-layer.
- Various modalities have been proposed and used for monitoring additive manufacturing process parameters, component shape, heat transfer, and other relevant aspects and parameters.
- a first system for non- destructively evaluating components fabricated by additive manufacturing systems and processes for non-destructively evaluating components fabricated by additive manufacturing includes a sensor array that is embedded within an electromagnetic field concentrating material or matrix, wherein the sensor array includes a plurality of individual elements arranged in a predetermined pattern for allowing substantially uniform coverage of an area of an electrically conductive component to be evaluated; wherein each element in the plurality of elements further includes at least one coil that acts as an exciter coil for generating an alternating electromagnetic field when activated, or a receiver coil for measuring a change in impedance of the at least one coil, or as both an exciter coil and a receiver coil; wherein the alternating electromagnetic field induces eddy currents in the component to be evaluated; and wherein the individual elements in the sensor array are excited in a predetermined sequence during a single pass of the sensor array over the area to be evaluated.
- a second system for non-destructively evaluating components fabricated by additive manufacturing systems and processes for non-destructively evaluating components fabricated by additive manufacturing includes a sensor array embedded within an electromagnetic field concentrating material or matrix, wherein the sensor array includes a plurality of individual elements arranged in a predetermined pattern for allowing substantially uniform coverage of an area of an electrically conductive component to be evaluated; wherein each element in the plurality of elements further includes at least one coil that acts as an exciter coil for generating an alternating electromagnetic field when activated, or a receiver coil for measuring a change in impedance of the at least one coil, or as both an exciter coil and a receiver coil; wherein the alternating electromagnetic field induces eddy currents in the component to be evaluated; and wherein the individual elements in the sensor array are excited in a predetermined sequence during a single pass of the sensor array over the area to be evaluated; and a processor for receiving and characterizing data gathered by the sensor array,
- a third system for non- destructively evaluating components fabricated by additive manufacturing systems and processes for non-destructively evaluating components fabricated by additive manufacturing includes a sensor array embedded within an electromagnetic field concentrating material or matrix, wherein the sensor array includes a plurality of individual elements arranged in a staggered pattern for allowing substantially uniform coverage of an area of an electrically conductive component to be evaluated; wherein each element in the plurality of elements further includes at least one coil that acts as an exciter coil for generating an alternating electromagnetic field when activated, or a receiver coil for measuring a change in impedance of the at least one coil, or as both an exciter coil and a receiver coil; wherein the alternating electromagnetic field induces eddy currents in the component to be evaluated; and wherein the individual elements in the sensor array are excited in a predetermined sequence during a single pass of the sensor array over the area to be evaluated; a processor for receiving and characterizing data gathered by the sensor array, where
- FIG. 1 is a bottom view of an electromagnetic sensor array in accordance with an exemplary embodiment of the present invention illustrating the placement of the individual coils within the array:
- FIG. 2 is a top view of an electromagnetic sensor array in accordance with an exemplary embodiment of the present invention illustrating the configuration of the connecting plate;
- FIG. 3 is flowchart illustrating the components and functionality of an NDE system using an electromagnetic sensor array, in accordance with an exemplary embodiment of the present invention
- FIG. 4 is flowchart illustrating the components and functionality of the front-end electronics of an NDE system using the electromagnetic sensor array of the present invention
- FIG. 5 is an illustration of an exemplary embodiment of the system of the present invention being used to evaluate a laser-powder bed fusion (L-PBF) process;
- L-PBF laser-powder bed fusion
- FIG. 6 is an illustration of the test coupon used with the electromagnetic sensor array of the present invention, wherein a series of notches or grooves have been formed in the test coupon;
- FIG. 7 is a graph showing signal magnitude at a notch depth of 160 ⁇ at layer
- FIG. 8 is a graph showing signal phase at a notch depth of 160 ⁇ at layer 29
- FIG. 9 is an illustration of the test coupon used with the electromagnetic sensor array of the present invention, wherein a large area of lack of fusion area (LOF) has been formed in the test coupon;
- LEF lack of fusion area
- FIG. 10 is a graph showing signal magnitude across the LOF area formed in the test coupon of FIG. 9 along the scan path of channel 19 of the electromagnetic sensor array of the present invention
- FIG. 11 is a graph showing signal phase across the LOF area formed in the test coupon of FIG. 9 along the scan path of channel 19 of the electromagnetic sensor array of the present invention
- FIG. 12 a graph showing signal magnitude away from the LOF area formed in the test coupon of FIG. 9 along the scan path of channel 26 of the electromagnetic sensor array of the present invention.
- FIG. 13 is a graph showing signal phase away from the LOF area formed in the test coupon of FIG. 9 along the scan path of channel 26 of the electromagnetic sensor array of the present invention.
- the present invention relates in general to non-destructive evaluation (NDE) techniques for use in manufacturing and more specifically to a NDE of components made by additive manufacturing (AM) processes using an array eddy current system and method.
- NDE non-destructive evaluation
- AM additive manufacturing
- This invention may be used for both process monitoring and NDE during and after fabrication.
- the disclosed sensor and NDE method significantly reduce post additive manufacturing NDE requirements by examining the entire volume of each layer for critical surface and subsurface discontinuities and or conditions with any orientation.
- the method of the present invention permits fast repair and re-examination of any such repair while the part being built is still in the device chamber and without the removal of powder (thereby reducing waste).
- electromagnetic sensor array 100 (which is shown in an inverted position) includes body 110, which further includes top portion 120 and bottom portion 130, which acts as a field concentrator.
- First row 140 of individual elements (or coils) 150 is arranged in a staggered, substantially parallel position relative to second row 160 of individual elements (or coils) 170. Staggering the rows of elements in this manner permits more uniform coverage of the inspected area on an AM component or part.
- each row includes 18 individual elements or coils for a total of 36 coils in the array. Other configurations are possible.
- FIG. 2 is a top view of an electromagnetic sensor array 200, which further includes a body 210 having a top portion 220 (that includes a printed circuit board) and a bottom portion 230.
- a first row of connectors 240 is positioned in parallel to a second row of connectors 260 in top portion 220.
- First and second wire leads 280 and 290 are also attached to top portion 220 and are shown in a flexed configuration.
- Array elements 150 and 170 are excited in a predetermined sequence while the entire array is scanned to cover the entire area of analysis in a single pass.
- an individual coil is excited, an alternating magnetic field is generated that then induces eddy currents in the AM component or part, if the AM component or part is electrically conductive.
- the density and distribution of eddy currents in the AM component or part being evaluated is dependent on material electromagnetic properties (e.g., magnetic permeability and electrical conductivity), electromagnetic field strength and frequency, geometry of the AM component or part, and the geometry of the element or coil generating the field.
- Changes in the eddy current electromagnetic field caused by changes in additive manufacturing material properties that affect electrical conductivity and/or magnetic permeability, presence of discontinuities and variations of distance between the sensor and inspected area (e.g., surface irregularity) will be registered with the same or different elements or coils of electromagnetic sensor array 100/200 (also referred to herein as an array eddy current (AEC) sensor.
- AEC array eddy current
- GMR magnetic field concentrating material
- AM components or parts are used as receivers in alternate embodiments of this invention.
- an electromagnetic field can be generated by a coil, or single or multiple conductors with a current to produce a field having maximum sensitivity for detecting discontinuities and conditions of interest in AM components or parts.
- the electromagnetic sensors of this invention also utilize magnetic field concentrating material for increasing sensitivity and resolution compared to conventional designs.
- FIG. 3 is flowchart illustrating the components and functionality of NDE system
- an electromagnetic sensor array is connected to a demultiplexer (DMux) and a multiplexer (Mux) for receiving an electrical signal from a generator, creating an electromagnetic field, and transmitting a measured signal containing information from an evaluated AM component or part for signal processing.
- the exemplary system shown in FIG. 3 includes electromagnetic sensor array 310, Mux 312, inbound preamplifier 314, lock-in amplifier 316, digital I/O 318, encoder 320, CPU 322, signal generator 324, outbound preamplifier 326, and DMux 328.
- Other configurations of this system are possible and are also aspects of the present invention.
- FIG. 4 is flowchart illustrating the components and functionality of front-end electronics 400 of an NDE system using the electromagnetic sensor array of the present invention.
- front-end electronics 400 consist of two main channels: working elements and reference elements.
- the working elements channel receives and transmits information from the AM component being evaluated while the reference element (coil positioned over good material) channel provides a signal that cancels any background detected from the material of the AM component and surrounding environment.
- the working elements and reference elements channels are connected in a bridge circuit, which provides improved sensitivity to changes detected in the properties of the materials being tested.
- Demultiplexer outputs and multiplexer inputs are buffered to improve circuit performance at high frequencies.
- front-end electronics 400 specifically include generator 410, which is connected to DMux 412, reference element 414, Mux 416, subtract junction 424, and processing device 426.
- Generator 410 is also connected to DMux 418, working element 420, Mux 422, subtract junction 424, and processing device 426.
- This configuration permits layer-by-layer examination and coverage of an area of interest with the minimum number of passes and precise positioning with respect to the additive manufacturing component top layer surface.
- the examination is conducted by following a laser or other fusion source when a single strip is deposited or after deposition of each layer to examine the entire surface and before application of powder for the next layer.
- Direct energy deposition layers and components can also be examined using the systems, devices, and methods of the present invention.
- FIG. 5 is an illustration of exemplary eddy current-based NDE system 500 being used to evaluate a laser-powder bed fusion (L-PBF) process, which utilizes metal powder 505.
- Electromagnetic sensor array 510 is mounted on scanner arm 512.
- Front-end electronics 514 are mounted inside the L-PBF chamber in close proximity to electromagnetic sensor array 510, thereby providing an improved signal to noise ratio and the ability to work at high frequencies by eliminating the undesirable effects on signal integrity associated with using long connecting cables between instruments.
- Temperature is measured at three locations with multiple thermal sensors: balance plate thermal sensor 516; reference element thermal sensor 518; thermal sensor 520, which is mounted in front of electromagnetic sensor array 510. Thermal data is analyzed together with measurements taken from the examiner layer to allow for precise thermal compensation of each layer measurement.
- Electromagnetic sensor array 510 is positioned over the balance plate of the L-PBF system, where data is acquired from intact material similar to the material to be tested. This information is used to null or balance the measurement channels before each examination of newly deposited layer. This eliminates or significantly reduces any effects that temperature may have on system electronics (e.g., gain drifts). Electromagnetic sensor array 510 will generate signal when a discontinuity (e.g. crack, LOF between neighboring, or side-by-side, or top-to-bottom solidified tracks, porosity), shape irregularity (e.g., large area LOF), or defect condition (e.g., alloy composition deviation, stress) is detected.
- a discontinuity e.g. crack, LOF between neighboring, or side-by-side, or top-to-bottom solidified tracks, porosity
- shape irregularity e.g., large area LOF
- defect condition e.g., alloy composition deviation, stress
- Eddy current-based NDE system 500 processes the discontinuity or condition signal and forwards a trigger signal to the L-PBF system or other additive manufacturing system.
- the additive manufacturing system then classifies the eddy current trigger signal and corrects the additive manufacturing process as necessary to eliminate the eddy current trigger signal (by ultimately rectifying the discontinuity or other condition of concern).
- the location and size of the eddy current indication is recorded and evaluated as being acceptable or unacceptable (i.e., rejected). If the indication is unacceptable, it is possible to reposition the system with electromagnetic sensor array 510, repair the location of concern, and reexamine the AM component or part.
- the described method can separate geometry and surface irregularity changes from material localized discontinuities and larger areas where material properties (e.g., stresses, phase and chemical composition, etc.) deviate from specifications if material property variations affect electrical conductivity and/or magnetic permeability.
- material properties e.g., stresses, phase and chemical composition, etc.
- the methods of this invention can be used for both process monitoring and NDE during and after fabrication.
- electromagnetic sensor array 510 was mounted on an XY-scanner arm to generate a C-scan view of an inspected area.
- a 20x20mm test coupon was built from Inconel 625 alloy using additive manufacturing.
- FIGS. 6 and 9 two test features were embedded sequentially in the test coupon in the Z-direction (i.e., height): (a) a series of five notches having different widths; and (ii) a large area of LOF.
- electromagnetic sensor array 600 was used to scan test coupon 610 along scan path 620 using channel 13 of electromagnetic sensor array 600.
- Notch design or desired width was 90 ⁇ , 180 ⁇ , 270 ⁇ , 450 ⁇ , and 900 ⁇ for notches 1, 2, 3, 4, and 5 respectively.
- the notches were built with increasing height or depth from layer 26 (L26) to layer 45 (L45). Each layer added about 40 ⁇ to notch depth. Data was acquired during the entire notch building process. Scanning data for one typical channel - channel 13 is shown in FIGS. 7-8 for L29 and L44. The shallow and narrow notches at L29 are more effectively detected on the phase plot (FIG.
- Notch signal magnitude and extent is also correlated to notch width and depth, which indicates the possibility for defect sizing.
- the surface of test coupon 610 started bulging around the wider notches due to heat transfer redistribution (see FIG. 7). The same affect was observed at edges of test coupon 610. After completing the notch build, 20 additional layers were deposited. The largest notch was also detectable as subsurface defect under several fused layers.
- electromagnetic sensor array 900 was used to scan test coupon 910 along scan path 930 using channel 19 of electromagnetic sensor array 900 and along scan path 940 using channel 26 of electromagnetic sensor array 900.
- Large (5x5mm) LOF area 920 was built from layer 67 (L67) to layer 75 (L75).
- the initial construction of test coupon 910 included building the lack of fusion area with a depth of 20 layers of material. However, the formation of a ridge or bulge near the LOF area edge caused re-coater to scrape the surface and the build process was stopped at L75. Surface area bulging was clearly detected well in advance of re-coater scraping (see FIG. 12). The scanning pattern and path of two array channels is shown in FIG. 9.
- FIGS. 10-11 which was gathered from channel 19, clearly indicates the presence and growth of lack of fusion depth.
- the lack of fusion area was also detected as a subsurface gap at L76 under two or three fused layers of material.
- the phase plot of FIG. 11 allows clear separation of surface (negative phase change) from subsurface (positive phase change) defects.
- the plots from channel 26 shown in FIGS. 12-13, away from the LOF area clearly indicate the surface bulging effect (see the magnitude plot of FIG. 12) during lac of fusion build and shortly thereafter.
- this invention includes the following features and advantageous.
- an electromagnetic sensor array includes a plurality of coils embedded in a field-concentrating media or matrix that greatly increases the intensity of the electromagnetic field near the coils resulting in improved resolution and sensitivity to discontinuities and conditions in AM components or parts being evaluated.
- two identical system channels (working and reference) in terms of electronic components that provide efficient cancellation of any background signal originating from the material being evaluated and surrounding environment. This aspect permits the system to amplify and process only signals which represent the difference between "good" or reference material and the material of the AM component or part being evaluated.
- the system corrects measurements taken from an AM component or part being evaluated by gathering and processing thermal data gathered from three separate locations within an active additive manufacturing system.
- the balance plate within the additive manufacturing device is used to provide a reference surface away from the AM component or part being evaluated to compensate for temperature effects and drifts during additive manufacturing builds having a long duration.
Abstract
Description
Claims
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201762509816P | 2017-05-23 | 2017-05-23 | |
PCT/US2018/033657 WO2018217626A1 (en) | 2017-05-23 | 2018-05-21 | Non-destructive evaluation of additive manufacturing components |
Publications (1)
Publication Number | Publication Date |
---|---|
EP3630409A1 true EP3630409A1 (en) | 2020-04-08 |
Family
ID=64396910
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP18806671.6A Withdrawn EP3630409A1 (en) | 2017-05-23 | 2018-05-21 | Non-destructive evaluation of additive manufacturing components |
Country Status (2)
Country | Link |
---|---|
EP (1) | EP3630409A1 (en) |
WO (1) | WO2018217626A1 (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN116539731B (en) * | 2023-07-06 | 2023-09-29 | 中国特种设备检测研究院 | Primary and secondary co-located transceiver transducer, imaging system and imaging method |
CN117368812B (en) * | 2023-12-08 | 2024-02-23 | 西南交通大学 | Method and device for measuring magnetic field intensity of high-temperature superconductive magnetic levitation transportation system |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6326780B1 (en) * | 1998-12-01 | 2001-12-04 | Visteon Global Technologies, Inc. | Magnetic field concentrator array for rotary position sensors |
US9279865B2 (en) * | 2012-05-09 | 2016-03-08 | Everspin Technologies, Inc. | Method and structure for testing and calibrating three axis magnetic field sensing devices |
US10786948B2 (en) * | 2014-11-18 | 2020-09-29 | Sigma Labs, Inc. | Multi-sensor quality inference and control for additive manufacturing processes |
US20160349215A1 (en) * | 2014-12-23 | 2016-12-01 | Edison Welding Institute, Inc. | Non-destructive evaluation of additive manufacturing components using an eddy current array system and method |
-
2018
- 2018-05-21 EP EP18806671.6A patent/EP3630409A1/en not_active Withdrawn
- 2018-05-21 WO PCT/US2018/033657 patent/WO2018217626A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2018217626A1 (en) | 2018-11-29 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US20160349215A1 (en) | Non-destructive evaluation of additive manufacturing components using an eddy current array system and method | |
JP4814511B2 (en) | Pulsed eddy current sensor probe and inspection method | |
US6952095B1 (en) | Surface mounted and scanning spatially periodic eddy-current sensor arrays | |
US6727691B2 (en) | High resolution inductive sensor arrays for material and defect characterization of welds | |
US20090315540A1 (en) | Primary windings having multiple parallel extended portions | |
US20050248339A1 (en) | Segmented field sensors | |
KR20150052865A (en) | Differential sensor, inspection system and method for the detection of anomalies in electrically conductive materials | |
US20180266993A1 (en) | Non-destructive evaluation of additive manufacturing components | |
EP3630409A1 (en) | Non-destructive evaluation of additive manufacturing components | |
US20160003775A1 (en) | Apparatus and Circuit | |
US7161351B2 (en) | Hidden feature characterization using a database of sensor responses | |
Pelkner et al. | Eddy current testing with high-spatial resolution probes using MR arrays as receiver | |
Angani et al. | Non-destructive testing of inclusions in cold-rolled strip steels using hall and giant magnetoresistance sensor arrays | |
Porto et al. | Design and analysis of a GMR eddy current probe for NDT | |
Schmidt et al. | A Portable Microwave Scanning Technique for Nondestructive Testing of Multi layered Dielectric Materials | |
Washabaugh et al. | Shaped-field eddy-current sensors and arrays | |
US20060202688A1 (en) | Detection system and method thereof | |
KR101056763B1 (en) | Manufacturing method of micro flaw flaw detector and sensor part | |
Espy et al. | Non-destructive evaluation with a linear array of 11 HTS SQUIDs | |
Flores et al. | Failure analysis of automotive ultrasonic parking sensors by X ray computed Tomography | |
Murner et al. | Buried corrosion detection in multi-layer airframe structures using pulsed eddy current | |
US20140091784A1 (en) | Artificial Defect for Eddy Current Inspection | |
Heuer et al. | Thin film characterization using high frequency eddy current spectroscopy | |
Nelson et al. | JSNDI_2002_nelson, ciji. | |
Flores et al. | Failure analysis of automotive ultrasonic parking sensors |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE |
|
PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE |
|
17P | Request for examination filed |
Effective date: 20191114 |
|
AK | Designated contracting states |
Kind code of ref document: A1 Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR |
|
AX | Request for extension of the european patent |
Extension state: BA ME |
|
DAV | Request for validation of the european patent (deleted) | ||
DAX | Request for extension of the european patent (deleted) | ||
STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN |
|
18D | Application deemed to be withdrawn |
Effective date: 20201201 |