TR
EN
Predicting Fatigue Life of A Mount of A Device with Shock Absorber
Öz
All aircraft operate under vibration loads and these loads cause vibration-induced fatigue damage to the parts. Fatigue damages are dangerous because they occur suddenly without giving a warning before, for this reason they need to be carefully analyzed. In the analysis, especially the natural frequencies and dampings must be determined correctly, because when the vibration loads match with the natural frequencies, resonance is observed and this reduces the life of the part. In this study, the fatigue life of a mount of a device with shock absorber is investigated. Flight tests were carried out in real flight scenarios to provide an input for the analysis. A modal test was performed to model the shock absorbers correctly. Vibration test was performed to prove the accuracy of the prepared finite element model and to determine the damping ratios. Fatigue analyses were performed in frequency domain with a commercial software, nCode, and the accuracy of the analysis was proven by the experiment.
Anahtar Kelimeler
Kaynakça
- [1] MIL-HDBK-5J, “Metallic Materials and Elements for Aerospace Vehicle Structures”, (2003).
- [1] MIL-HDBK-5J, “Metallic Materials and Elements for Aerospace Vehicle Structures”, (2003).
- [2] Albert W.A.J., “Uber Treibseile am Harz.”, Archiv fur Mineralogie, Georgnosie, Bergbau und Huttenkunde, Berlin, (1837).
- [2] Albert W.A.J., “Uber Treibseile am Harz.”, Archiv fur Mineralogie, Georgnosie, Bergbau und Huttenkunde, Berlin, (1837).
- [3] https://en.wikipedia.org/wiki/Fatigue_(material),
- [3] https://en.wikipedia.org/wiki/Fatigue_(material),
- [4] Rankine W.J.M., “On the causes of the unexpected breakage of the journals of railway axles, and on the means of preventing such accidents by observing the law of continuity in their construction”, Journal of the Franklin Institute, 36: 178-180, (1843).
- [4] Rankine W.J.M., “On the causes of the unexpected breakage of the journals of railway axles, and on the means of preventing such accidents by observing the law of continuity in their construction”, Journal of the Franklin Institute, 36: 178-180, (1843).
Ayrıntılar
Birincil Dil
İngilizce
Konular
Mühendislik
Bölüm
Araştırma Makalesi
Erken Görünüm Tarihi
27 Mart 2024
Yayımlanma Tarihi
25 Temmuz 2024
Gönderilme Tarihi
28 Kasım 2022
Kabul Tarihi
25 Aralık 2022
Yayımlandığı Sayı
Yıl 2024 Cilt: 27 Sayı: 3
APA
Tekeci, U., & Yıldırım, B. (2024). Predicting Fatigue Life of A Mount of A Device with Shock Absorber. Politeknik Dergisi, 27(3), 1005-1015. https://doi.org/10.2339/politeknik.1210934
AMA
1.Tekeci U, Yıldırım B. Predicting Fatigue Life of A Mount of A Device with Shock Absorber. Politeknik Dergisi. 2024;27(3):1005-1015. doi:10.2339/politeknik.1210934
Chicago
Tekeci, Uğur, ve Bora Yıldırım. 2024. “Predicting Fatigue Life of A Mount of A Device with Shock Absorber”. Politeknik Dergisi 27 (3): 1005-15. https://doi.org/10.2339/politeknik.1210934.
EndNote
Tekeci U, Yıldırım B (01 Temmuz 2024) Predicting Fatigue Life of A Mount of A Device with Shock Absorber. Politeknik Dergisi 27 3 1005–1015.
IEEE
[1]U. Tekeci ve B. Yıldırım, “Predicting Fatigue Life of A Mount of A Device with Shock Absorber”, Politeknik Dergisi, c. 27, sy 3, ss. 1005–1015, Tem. 2024, doi: 10.2339/politeknik.1210934.
ISNAD
Tekeci, Uğur - Yıldırım, Bora. “Predicting Fatigue Life of A Mount of A Device with Shock Absorber”. Politeknik Dergisi 27/3 (01 Temmuz 2024): 1005-1015. https://doi.org/10.2339/politeknik.1210934.
JAMA
1.Tekeci U, Yıldırım B. Predicting Fatigue Life of A Mount of A Device with Shock Absorber. Politeknik Dergisi. 2024;27:1005–1015.
MLA
Tekeci, Uğur, ve Bora Yıldırım. “Predicting Fatigue Life of A Mount of A Device with Shock Absorber”. Politeknik Dergisi, c. 27, sy 3, Temmuz 2024, ss. 1005-1, doi:10.2339/politeknik.1210934.
Vancouver
1.Uğur Tekeci, Bora Yıldırım. Predicting Fatigue Life of A Mount of A Device with Shock Absorber. Politeknik Dergisi. 01 Temmuz 2024;27(3):1005-1. doi:10.2339/politeknik.1210934
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