دورية أكاديمية
Research on Transfer Characteristics of Engine Vibration Load to Cabin Seat
| العنوان: | Research on Transfer Characteristics of Engine Vibration Load to Cabin Seat |
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| المصدر: | Xibei Gongye Daxue Xuebao, Vol 38, Iss 6, Pp 1163-1170 (2020) |
| بيانات النشر: | EDP Sciences, 2020. |
| سنة النشر: | 2020 |
| المجموعة: | LCC:Motor vehicles. Aeronautics. Astronautics |
| مصطلحات موضوعية: | engine vibration, otpa, vibration isolation, vibration contribution, load transmission, Motor vehicles. Aeronautics. Astronautics, TL1-4050 |
| الوصف: | Aeroengine is one of the main vibration sources that affect the passenger comfort. The contribution of engine vibration to the vibration response of seat will provide basic data for the design of airliner vibration comfort and engine vibration isolation installation. Firstly, the dynamical model of middle fuselage compartment with double-beam wing was established. Then, based on the typical vibration load spectrum of the engine, the acceleration responses of the key nodes of the wing beam and the seat connection points were analyzed, and the main path of engine vibration transmission to seats was identified. Finally, using operational transfer path analysis (OTPA) method, the contribution of engine front and rear mount point vibration to the vertical acceleration response of the seats was compared, and the three-dimensional information of wing structure vibration transmission was explored. The results show that the fundamental frequency component of low-pressure rotor of engine vibration has the greatest impact on the seat vertical response under takeoff and cruise conditions, the contribution rate of the front mount point vibration is about 71% and 67% respectively. However, the fundamental and its 3/2 times frequency components of high-pressure rotor have relatively large impact on the seats vertical response under flight idle state, and the contribution rate of engine front mount point vibration is about 45% and 60% respectively. In addition, the engine vibration is mainly transmitted from the wing front beam to the seat vertical response. The vertical direction of the wing beam and the rotation direction around the fuselage are also the main direction of vibration transmission. |
| نوع الوثيقة: | article |
| وصف الملف: | electronic resource |
| اللغة: | Chinese |
| تدمد: | 1000-2758 2609-7125 20203861 |
| Relation: | https://www.jnwpu.org/articles/jnwpu/full_html/2020/06/jnwpu2020386p1163/jnwpu2020386p1163.html; https://doaj.org/toc/1000-2758; https://doaj.org/toc/2609-7125 |
| DOI: | 10.1051/jnwpu/20203861163 |
| URL الوصول: | https://doaj.org/article/0496017f2ee349299b88d9f81b0bb25e |
| رقم الأكسشن: | edsdoj.0496017f2ee349299b88d9f81b0bb25e |
| قاعدة البيانات: | Directory of Open Access Journals |
Full Text Finder | تدمد: | 10002758 26097125 20203861 |
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| DOI: | 10.1051/jnwpu/20203861163 |