TY - GEN
T1 - Dynali H3 Helicopter Tubular Frame Chassis Static Structural Analysis
AU - Al Shamsi, Mouza
AU - Al Darmaki, Afra
AU - Al Shamsi, Aysha Rashed
AU - Al Khateri, Mohammed
AU - Seyedzadeh, Ameereh
AU - Mourad, Abdel Hamid Ismail
N1 - Publisher Copyright:
© 2022 IEEE.
PY - 2022
Y1 - 2022
N2 - The design and development of a vehicle chassis is of a high significance in the aviation industry. This is due to its vital role in supporting the main structure of the vehicle in both static and dynamic conditions. It provides enough space to carry the various components of the vehicle. Therefore, it should be strong enough to withstand the different types of stresses. In current work, the tubular frame chassis of Dynali H3 2-seater helicopter is modeled with CATIA V5 and simulated using Ansys Static Structural Software by implying Finite Element Analysis (FEA) method. The main aim of this work is to perform structural analysis on the existing frame using the derived static loading acting on the tubular frame. The analysis focused on the structural loading using static loading only aiming at improving the tubular spaceframe chassis strength and design integrity of the current model in such a way that stresses are minimum, and the performance is maximum. The proposed design experienced less deformation and stresses compared to the current frame under the same static loading.
AB - The design and development of a vehicle chassis is of a high significance in the aviation industry. This is due to its vital role in supporting the main structure of the vehicle in both static and dynamic conditions. It provides enough space to carry the various components of the vehicle. Therefore, it should be strong enough to withstand the different types of stresses. In current work, the tubular frame chassis of Dynali H3 2-seater helicopter is modeled with CATIA V5 and simulated using Ansys Static Structural Software by implying Finite Element Analysis (FEA) method. The main aim of this work is to perform structural analysis on the existing frame using the derived static loading acting on the tubular frame. The analysis focused on the structural loading using static loading only aiming at improving the tubular spaceframe chassis strength and design integrity of the current model in such a way that stresses are minimum, and the performance is maximum. The proposed design experienced less deformation and stresses compared to the current frame under the same static loading.
KW - Chassis
KW - finite element analysis
KW - space frame
KW - stress
KW - tubular frame
UR - http://www.scopus.com/inward/record.url?scp=85128383227&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=85128383227&partnerID=8YFLogxK
U2 - 10.1109/ASET53988.2022.9734844
DO - 10.1109/ASET53988.2022.9734844
M3 - Conference contribution
AN - SCOPUS:85128383227
T3 - 2022 Advances in Science and Engineering Technology International Conferences, ASET 2022
BT - 2022 Advances in Science and Engineering Technology International Conferences, ASET 2022
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2022 Advances in Science and Engineering Technology International Conferences, ASET 2022
Y2 - 21 February 2022 through 24 February 2022
ER -
