Kamali, Seyed Mohammad, Nouri, Ali, Mohammad Khanlo, Heshmatallah, Sabouri, Hadi. (1404). Investigating the Effect of Seat Suspension System and Cushion on the Dynamic Behavior of the 214 Helicopter Pilot's Body. نشریه مهندسی عمران امیرکبیر, 9(4), 431-446. doi: 10.22060/ajme.2025.23838.6161
Seyed Mohammad Kamali; Ali Nouri; Heshmatallah Mohammad Khanlo; Hadi Sabouri. "Investigating the Effect of Seat Suspension System and Cushion on the Dynamic Behavior of the 214 Helicopter Pilot's Body". نشریه مهندسی عمران امیرکبیر, 9, 4, 1404, 431-446. doi: 10.22060/ajme.2025.23838.6161
Kamali, Seyed Mohammad, Nouri, Ali, Mohammad Khanlo, Heshmatallah, Sabouri, Hadi. (1404). 'Investigating the Effect of Seat Suspension System and Cushion on the Dynamic Behavior of the 214 Helicopter Pilot's Body', نشریه مهندسی عمران امیرکبیر, 9(4), pp. 431-446. doi: 10.22060/ajme.2025.23838.6161
Kamali, Seyed Mohammad, Nouri, Ali, Mohammad Khanlo, Heshmatallah, Sabouri, Hadi. Investigating the Effect of Seat Suspension System and Cushion on the Dynamic Behavior of the 214 Helicopter Pilot's Body. نشریه مهندسی عمران امیرکبیر, 1404; 9(4): 431-446. doi: 10.22060/ajme.2025.23838.6161

Investigating the Effect of Seat Suspension System and Cushion on the Dynamic Behavior of the 214 Helicopter Pilot's Body

AUT Journal of Mechanical Engineering
دوره 9، شماره 4، زمستان 2025، صفحه 431-446    اصل مقاله (1.96 M)
نوع مقاله: Research Article
شناسه دیجیتال (DOI): 10.22060/ajme.2025.23838.6161
نویسندگان
Seyed Mohammad Kamali1؛ Ali Nouri* 1؛ Heshmatallah Mohammad Khanlo1؛ Hadi Sabouri2
1Department of Aerospace Engineering, Shahid Sattari Aeronautical University of Science and Technology, Tehran, Iran
2Department of Mechanical Engineering, Faculty of Engineering, Kharazmi University, Tehran, Iran
چکیده
In this study, the influence of the stiffness and damping characteristics of the pilot seat cushion in the Bell 214 helicopter is investigated as two critical factors in reducing the transmission of vibrations to the pilot’s body. Since the dominant vibrations in the Bell 214 occur at low frequencies, typically between 2 and 15 Hz, the seat suspension system is not effective in this range, and the seat cushion plays a more significant role in vibration isolation. First, the biodynamic response of the human body is validated by comparing the results with existing experimental and analytical data related to helicopter vibration exposure. Then, the biodynamic equations of motion are analyzed using a four-degree-of-freedom seated human model under various configurations, with and without suspension and seat cushioning. Finally, the frequency domain response is examined through three-dimensional plots to evaluate the effect of different cushion stiffness and damping values. The results indicate that selecting optimal mechanical properties for the cushion can significantly enhance pilot comfort and play an effective role in reducing vibration-induced physical injuries.
کلیدواژه‌ها
Ride Comfort؛ Cushion؛ Transmissibility؛ Mechanical Impedance؛ Apparent Mass
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