Web Optimization of Compression Ignition Aviation Engine Crankshaft
The focus of this study was the weight reduction of crankshaft web regions of an inline 4 cylinder, 250 HP compression ignition engine with a combustion chamber volume of 2499 cm3 intended for use in aircraft. Iteration #0 model was generated by manual reduction of a reference model. According to th...
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| Main Authors: | , , , , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Wiley
2022-01-01
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| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2022/7976691 |
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| _version_ | 1832563324395454464 |
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| author | Serkan Galata Yiğit Okur Ülkü Uzan Emre Ünlü Kudret Muhziroğlu Övün Işın Mehmet Oğuz Turgut Emin Tuzlu |
| author_facet | Serkan Galata Yiğit Okur Ülkü Uzan Emre Ünlü Kudret Muhziroğlu Övün Işın Mehmet Oğuz Turgut Emin Tuzlu |
| author_sort | Serkan Galata |
| collection | DOAJ |
| description | The focus of this study was the weight reduction of crankshaft web regions of an inline 4 cylinder, 250 HP compression ignition engine with a combustion chamber volume of 2499 cm3 intended for use in aircraft. Iteration #0 model was generated by manual reduction of a reference model. According to the results of the analyses, the stresses were compared. Since the increase in stress values of weight reduced model over the reference model exceeded the targeted upper limit of 15.0%, three geometric parameters have been defined, and seven candidate design models have been created by using one, two, or all of the three parameters. In order to maximize the weight reduction by achieving the target stress limit, the lightest design model was obtained in the 10th iteration. For the last three iterations, new parametric values were determined by utilizing the calculated effects of the geometric parameters on stress and weight. |
| format | Article |
| id | doaj-art-e5b7231340e44a559a0e1084b82a35b2 |
| institution | Kabale University |
| issn | 1687-5974 |
| language | English |
| publishDate | 2022-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Aerospace Engineering |
| spelling | doaj-art-e5b7231340e44a559a0e1084b82a35b22025-02-03T01:20:35ZengWileyInternational Journal of Aerospace Engineering1687-59742022-01-01202210.1155/2022/7976691Web Optimization of Compression Ignition Aviation Engine CrankshaftSerkan Galata0Yiğit Okur1Ülkü Uzan2Emre Ünlü3Kudret Muhziroğlu4Övün Işın5Mehmet Oğuz Turgut6Emin Tuzlu7TUSAŞ Engine Industries Inc.TUSAŞ Engine Industries Inc.TUSAŞ Engine Industries Inc.TUSAŞ Engine Industries Inc.TUSAŞ Engine Industries Inc.Yildiz Technical UniversityTUSAŞ Engine Industries Inc.TUSAŞ Engine Industries Inc.The focus of this study was the weight reduction of crankshaft web regions of an inline 4 cylinder, 250 HP compression ignition engine with a combustion chamber volume of 2499 cm3 intended for use in aircraft. Iteration #0 model was generated by manual reduction of a reference model. According to the results of the analyses, the stresses were compared. Since the increase in stress values of weight reduced model over the reference model exceeded the targeted upper limit of 15.0%, three geometric parameters have been defined, and seven candidate design models have been created by using one, two, or all of the three parameters. In order to maximize the weight reduction by achieving the target stress limit, the lightest design model was obtained in the 10th iteration. For the last three iterations, new parametric values were determined by utilizing the calculated effects of the geometric parameters on stress and weight.http://dx.doi.org/10.1155/2022/7976691 |
| spellingShingle | Serkan Galata Yiğit Okur Ülkü Uzan Emre Ünlü Kudret Muhziroğlu Övün Işın Mehmet Oğuz Turgut Emin Tuzlu Web Optimization of Compression Ignition Aviation Engine Crankshaft International Journal of Aerospace Engineering |
| title | Web Optimization of Compression Ignition Aviation Engine Crankshaft |
| title_full | Web Optimization of Compression Ignition Aviation Engine Crankshaft |
| title_fullStr | Web Optimization of Compression Ignition Aviation Engine Crankshaft |
| title_full_unstemmed | Web Optimization of Compression Ignition Aviation Engine Crankshaft |
| title_short | Web Optimization of Compression Ignition Aviation Engine Crankshaft |
| title_sort | web optimization of compression ignition aviation engine crankshaft |
| url | http://dx.doi.org/10.1155/2022/7976691 |
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