Given the increasing necessity of improving the structural assembly methods especially in the aviation industry; a proper study by comparison of the currently used methods could reveal to be helpful in choosing the right method to achieve one’s manufacturing goals. It could also incite further researches to solve the existing deficiencies in this domain or make more efficient the existing ones. With the above-mentioned motives, this paper is a close look at dimpling methods. This paper will revise the key characteristics of hot dimpling and cold dimpling by experimental results on sheet materials with different properties. Tensile test and shear test were carried out to evaluate the strength of the sheet material after each dimpling method and study diverse failures remarked while doing experiments. The dimples’ status, fatigue and especially radial cracks and hole sizes, is evaluated. We wish to achieve dimples that permit the rivets to sit flush with the surface of the surrounding material and rivet’s head to fit with no defect. Due to the increasing complexities encountered in the manufacturing and assembly of air and space vehicles, missile systems and associated equipment, this research is provided to be used as an enlightenment to dimpling processes; especially ram coin dimpling. The ram coin dimpling method is divided into cold dimpling (room temperature) and hot dimpling (increased temperature). Comparing this research paper to the studies previously done, we found that hot dimpling though requiring a lot more attention proves to be more efficient on thick or brittle sheet materials, where cold dimpling would produce radial cracks.
Published in | International Journal of Mechanical Engineering and Applications (Volume 9, Issue 3) |
DOI | 10.11648/j.ijmea.20210903.11 |
Page(s) | 42-49 |
Creative Commons |
This is an Open Access article, distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution and reproduction in any medium or format, provided the original work is properly cited. |
Copyright |
Copyright © The Author(s), 2021. Published by Science Publishing Group |
Ram Coin Dimpling, Countersinking, Riveting, Sheet Material, Deburring, Tensile Test
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APA Style
Ishimwe Irene Fidele. (2021). Ram Coin Dimpling: Assessment of Modern Dimpling Methods. International Journal of Mechanical Engineering and Applications, 9(3), 42-49. https://doi.org/10.11648/j.ijmea.20210903.11
ACS Style
Ishimwe Irene Fidele. Ram Coin Dimpling: Assessment of Modern Dimpling Methods. Int. J. Mech. Eng. Appl. 2021, 9(3), 42-49. doi: 10.11648/j.ijmea.20210903.11
AMA Style
Ishimwe Irene Fidele. Ram Coin Dimpling: Assessment of Modern Dimpling Methods. Int J Mech Eng Appl. 2021;9(3):42-49. doi: 10.11648/j.ijmea.20210903.11
@article{10.11648/j.ijmea.20210903.11, author = {Ishimwe Irene Fidele}, title = {Ram Coin Dimpling: Assessment of Modern Dimpling Methods}, journal = {International Journal of Mechanical Engineering and Applications}, volume = {9}, number = {3}, pages = {42-49}, doi = {10.11648/j.ijmea.20210903.11}, url = {https://doi.org/10.11648/j.ijmea.20210903.11}, eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.ijmea.20210903.11}, abstract = {Given the increasing necessity of improving the structural assembly methods especially in the aviation industry; a proper study by comparison of the currently used methods could reveal to be helpful in choosing the right method to achieve one’s manufacturing goals. It could also incite further researches to solve the existing deficiencies in this domain or make more efficient the existing ones. With the above-mentioned motives, this paper is a close look at dimpling methods. This paper will revise the key characteristics of hot dimpling and cold dimpling by experimental results on sheet materials with different properties. Tensile test and shear test were carried out to evaluate the strength of the sheet material after each dimpling method and study diverse failures remarked while doing experiments. The dimples’ status, fatigue and especially radial cracks and hole sizes, is evaluated. We wish to achieve dimples that permit the rivets to sit flush with the surface of the surrounding material and rivet’s head to fit with no defect. Due to the increasing complexities encountered in the manufacturing and assembly of air and space vehicles, missile systems and associated equipment, this research is provided to be used as an enlightenment to dimpling processes; especially ram coin dimpling. The ram coin dimpling method is divided into cold dimpling (room temperature) and hot dimpling (increased temperature). Comparing this research paper to the studies previously done, we found that hot dimpling though requiring a lot more attention proves to be more efficient on thick or brittle sheet materials, where cold dimpling would produce radial cracks.}, year = {2021} }
TY - JOUR T1 - Ram Coin Dimpling: Assessment of Modern Dimpling Methods AU - Ishimwe Irene Fidele Y1 - 2021/08/13 PY - 2021 N1 - https://doi.org/10.11648/j.ijmea.20210903.11 DO - 10.11648/j.ijmea.20210903.11 T2 - International Journal of Mechanical Engineering and Applications JF - International Journal of Mechanical Engineering and Applications JO - International Journal of Mechanical Engineering and Applications SP - 42 EP - 49 PB - Science Publishing Group SN - 2330-0248 UR - https://doi.org/10.11648/j.ijmea.20210903.11 AB - Given the increasing necessity of improving the structural assembly methods especially in the aviation industry; a proper study by comparison of the currently used methods could reveal to be helpful in choosing the right method to achieve one’s manufacturing goals. It could also incite further researches to solve the existing deficiencies in this domain or make more efficient the existing ones. With the above-mentioned motives, this paper is a close look at dimpling methods. This paper will revise the key characteristics of hot dimpling and cold dimpling by experimental results on sheet materials with different properties. Tensile test and shear test were carried out to evaluate the strength of the sheet material after each dimpling method and study diverse failures remarked while doing experiments. The dimples’ status, fatigue and especially radial cracks and hole sizes, is evaluated. We wish to achieve dimples that permit the rivets to sit flush with the surface of the surrounding material and rivet’s head to fit with no defect. Due to the increasing complexities encountered in the manufacturing and assembly of air and space vehicles, missile systems and associated equipment, this research is provided to be used as an enlightenment to dimpling processes; especially ram coin dimpling. The ram coin dimpling method is divided into cold dimpling (room temperature) and hot dimpling (increased temperature). Comparing this research paper to the studies previously done, we found that hot dimpling though requiring a lot more attention proves to be more efficient on thick or brittle sheet materials, where cold dimpling would produce radial cracks. VL - 9 IS - 3 ER -