Qualification of Additive Manufacturing Flaw Fabrication Process for Verification of X-ray Computed Tomography of Complex Geometry Components Article Swipe
Evgueni Todorov
,
Mahdi Jamshidinia
,
S. M. Kelly
,
Scott Newhouse
,
Jeffrey Urbanski
,
Christopher Allison
·
YOU?
·
· 2016
· Open Access
·
YOU?
·
· 2016
· Open Access
·
Nondestructive Evaluation (NDE) techniques are needed to validate the additive manufacturing (AM) process performance. The lack of adequate NDE techniques for examination before, during and after AM component fabrication was identified as one of the main current challenges [1]. X-ray computed tomography (CT) was selected as primary technique for post-process inspection of components with complex shapes where the advantages of AM are fully realized [2]. To establish an initial baseline of CT data, Direct Metal Laser Melting (DMLM) and Electron Beam Melting (EBM) were used to fabricate coupons and complex geometry aerospace components with typical flaws and conditions. A flaw matrix was designed and the two processes were optimized to produce the desired flaws necessary for verification of CT performance in Inconel 718 and Ti-6Al-4V. Four coupon batches were fabricated. Surface and subsurface flaws were implanted such as pores, up to 135 AM process induced, and 8 machined artificial flaws. All four batches were CT inspected to measure the flaws and compare with the matrix to qualify the flaw fabrication process and determine the range of flaws that could reliably be produced. Coupons were sectioned to verify the CT measurements. CT data showed residual powder and differences between surface and subsurface flaw morphology. Results will be used in subsequent phases of the project to build and CT inspect components with complex shape and geometry for establishing CT baseline capabilities.
Related Topics
Concepts
Fabrication
Process (computing)
Computed tomography
Engineering drawing
Manufacturing process
Tomography
Geometry
X-ray
Materials science
Mechanical engineering
Computer science
Engineering
Mathematics
Composite material
Optics
Physics
Programming language
Medicine
Pathology
Radiology
Alternative medicine
Metadata
- Type
- article
- Language
- en
- Landing Page
- https://lib.dr.iastate.edu/qnde/2016/abstracts/254
- https://lib.dr.iastate.edu/cgi/viewcontent.cgi?article=4899&context=qnde
- OA Status
- green
- Related Works
- 20
- OpenAlex ID
- https://openalex.org/W2572727384
All OpenAlex metadata
Raw OpenAlex JSON
- OpenAlex ID
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https://openalex.org/W2572727384Canonical identifier for this work in OpenAlex
- Title
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Qualification of Additive Manufacturing Flaw Fabrication Process for Verification of X-ray Computed Tomography of Complex Geometry ComponentsWork title
- Type
-
articleOpenAlex work type
- Language
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enPrimary language
- Publication year
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2016Year of publication
- Publication date
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2016-01-01Full publication date if available
- Authors
-
Evgueni Todorov, Mahdi Jamshidinia, S. M. Kelly, Scott Newhouse, Jeffrey Urbanski, Christopher AllisonList of authors in order
- Landing page
-
https://lib.dr.iastate.edu/qnde/2016/abstracts/254Publisher landing page
- PDF URL
-
https://lib.dr.iastate.edu/cgi/viewcontent.cgi?article=4899&context=qndeDirect link to full text PDF
- Open access
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YesWhether a free full text is available
- OA status
-
greenOpen access status per OpenAlex
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https://lib.dr.iastate.edu/cgi/viewcontent.cgi?article=4899&context=qndeDirect OA link when available
- Concepts
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Fabrication, Process (computing), Computed tomography, Engineering drawing, Manufacturing process, Tomography, Geometry, X-ray, Materials science, Mechanical engineering, Computer science, Engineering, Mathematics, Composite material, Optics, Physics, Programming language, Medicine, Pathology, Radiology, Alternative medicineTop concepts (fields/topics) attached by OpenAlex
- Cited by
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0Total citation count in OpenAlex
- Related works (count)
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20Other works algorithmically related by OpenAlex
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| abstract_inverted_index.flaw | 99, 168, 201 |
| abstract_inverted_index.four | 151 |
| abstract_inverted_index.lack | 15 |
| abstract_inverted_index.main | 35 |
| abstract_inverted_index.such | 136 |
| abstract_inverted_index.that | 177 |
| abstract_inverted_index.used | 84, 206 |
| abstract_inverted_index.were | 83, 107, 128, 134, 153, 183 |
| abstract_inverted_index.will | 204 |
| abstract_inverted_index.with | 53, 93, 162, 219 |
| abstract_inverted_index.(EBM) | 82 |
| abstract_inverted_index.(NDE) | 2 |
| abstract_inverted_index.Laser | 75 |
| abstract_inverted_index.Metal | 74 |
| abstract_inverted_index.X-ray | 39 |
| abstract_inverted_index.after | 25 |
| abstract_inverted_index.build | 214 |
| abstract_inverted_index.could | 178 |
| abstract_inverted_index.data, | 72 |
| abstract_inverted_index.flaws | 95, 113, 133, 159, 176 |
| abstract_inverted_index.fully | 62 |
| abstract_inverted_index.range | 174 |
| abstract_inverted_index.shape | 221 |
| abstract_inverted_index.where | 56 |
| abstract_inverted_index.(DMLM) | 77 |
| abstract_inverted_index.Direct | 73 |
| abstract_inverted_index.coupon | 126 |
| abstract_inverted_index.during | 23 |
| abstract_inverted_index.flaws. | 149 |
| abstract_inverted_index.matrix | 100, 164 |
| abstract_inverted_index.needed | 5 |
| abstract_inverted_index.phases | 209 |
| abstract_inverted_index.pores, | 138 |
| abstract_inverted_index.powder | 194 |
| abstract_inverted_index.shapes | 55 |
| abstract_inverted_index.showed | 192 |
| abstract_inverted_index.verify | 186 |
| abstract_inverted_index.Coupons | 182 |
| abstract_inverted_index.Inconel | 121 |
| abstract_inverted_index.Melting | 76, 81 |
| abstract_inverted_index.Results | 203 |
| abstract_inverted_index.Surface | 130 |
| abstract_inverted_index.batches | 127, 152 |
| abstract_inverted_index.before, | 22 |
| abstract_inverted_index.between | 197 |
| abstract_inverted_index.compare | 161 |
| abstract_inverted_index.complex | 54, 89, 220 |
| abstract_inverted_index.coupons | 87 |
| abstract_inverted_index.current | 36 |
| abstract_inverted_index.desired | 112 |
| abstract_inverted_index.initial | 68 |
| abstract_inverted_index.inspect | 217 |
| abstract_inverted_index.measure | 157 |
| abstract_inverted_index.primary | 46 |
| abstract_inverted_index.process | 12, 143, 170 |
| abstract_inverted_index.produce | 110 |
| abstract_inverted_index.project | 212 |
| abstract_inverted_index.qualify | 166 |
| abstract_inverted_index.surface | 198 |
| abstract_inverted_index.typical | 94 |
| abstract_inverted_index.Electron | 79 |
| abstract_inverted_index.additive | 9 |
| abstract_inverted_index.adequate | 17 |
| abstract_inverted_index.baseline | 69, 227 |
| abstract_inverted_index.computed | 40 |
| abstract_inverted_index.designed | 102 |
| abstract_inverted_index.geometry | 90, 223 |
| abstract_inverted_index.induced, | 144 |
| abstract_inverted_index.machined | 147 |
| abstract_inverted_index.realized | 63 |
| abstract_inverted_index.reliably | 179 |
| abstract_inverted_index.residual | 193 |
| abstract_inverted_index.selected | 44 |
| abstract_inverted_index.validate | 7 |
| abstract_inverted_index.aerospace | 91 |
| abstract_inverted_index.component | 27 |
| abstract_inverted_index.determine | 172 |
| abstract_inverted_index.establish | 66 |
| abstract_inverted_index.fabricate | 86 |
| abstract_inverted_index.implanted | 135 |
| abstract_inverted_index.inspected | 155 |
| abstract_inverted_index.necessary | 114 |
| abstract_inverted_index.optimized | 108 |
| abstract_inverted_index.processes | 106 |
| abstract_inverted_index.produced. | 181 |
| abstract_inverted_index.sectioned | 184 |
| abstract_inverted_index.technique | 47 |
| abstract_inverted_index.Evaluation | 1 |
| abstract_inverted_index.Ti-6Al-4V. | 124 |
| abstract_inverted_index.advantages | 58 |
| abstract_inverted_index.artificial | 148 |
| abstract_inverted_index.challenges | 37 |
| abstract_inverted_index.components | 52, 92, 218 |
| abstract_inverted_index.identified | 30 |
| abstract_inverted_index.inspection | 50 |
| abstract_inverted_index.subsequent | 208 |
| abstract_inverted_index.subsurface | 132, 200 |
| abstract_inverted_index.techniques | 3, 19 |
| abstract_inverted_index.tomography | 41 |
| abstract_inverted_index.conditions. | 97 |
| abstract_inverted_index.differences | 196 |
| abstract_inverted_index.examination | 21 |
| abstract_inverted_index.fabricated. | 129 |
| abstract_inverted_index.fabrication | 28, 169 |
| abstract_inverted_index.morphology. | 202 |
| abstract_inverted_index.performance | 119 |
| abstract_inverted_index.establishing | 225 |
| abstract_inverted_index.performance. | 13 |
| abstract_inverted_index.post-process | 49 |
| abstract_inverted_index.verification | 116 |
| abstract_inverted_index.capabilities. | 228 |
| abstract_inverted_index.manufacturing | 10 |
| abstract_inverted_index.measurements. | 189 |
| abstract_inverted_index.Nondestructive | 0 |
| cited_by_percentile_year | |
| countries_distinct_count | 0 |
| institutions_distinct_count | 6 |
| citation_normalized_percentile.value | 0.17048618 |
| citation_normalized_percentile.is_in_top_1_percent | False |
| citation_normalized_percentile.is_in_top_10_percent | False |