New Design of Aircraft Seat Main Frame
作者： Vinsensius Tiara Putra , Rachmat Sriwijaya
DOI: 10.1109/ICST47872.2019.9166378
关键词:
摘要: Main frame structural strength of new aircraft seat was studied using simulation method. Structural considered by giving static loads to the structure based on emergency landing condition. Backward load 1.5 g, downward 6 forward 9 sideward 4 and upward 3 g applied structure. Safety factor 1.33 used as minimum safe value The results showed that safety backward, downward, forward, simulations were 8.37, 8.72, 1.39, 1.50, 14.02 respectively. Compare with other highest stress 232 MPa occurred in main under deformation condition 0.001 m. That indicated had no plastic deformation.
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