Elevated Skid Design for an Unmanned Disaster Relief Helicopter
DOI:
https://doi.org/10.24949/njes.v9i1.155Abstract
Development of unmanned disaster relief helicopters is need of developing countries like Pakistan to save the lives of disaster victims. As a part of research on the development of unmanned disaster relief helicopter at National University of Sciences and Technology (NUST), this paper aims to address the problems of installing disaster relief equipment on a Radio Controlled (RC) model helicopter. Skid elevation is essential in order to facilitate the installation of disaster surveying equipment like video and data telemetry system. This paper proposes an elevated skid design as a potential solution to the problem. The Structure of elevated skid has been simulated for the static structural analysis to check its safety and reliability. Simulation results and overall design of proposed elevated skid has been compared with the existing skids. Virtual Computer Aided Design (CAD) PRO-E has been used for the modeling of elevated skid and ANSYS has been used for the simulations of proposed design. Proposed elevated skid has been specifically designed for the 90 size model helicopters and can be utilized to attach the additional imagery and data telemetry equipment beneath the helicopter.References
E. Ackerman, “Japan earthquake: Global Hawk UAV may be able to peek inside damaged reactors,” IEEE Spectrum, vol. 17, 2011.
T.-Y. Chou, et al., Disaster monitoring and management by the unmanned aerial vehicle technology, na, 2010.
S. Tadokoro, “Special project on development of advanced robots for disaster response (DDT project),” Proc. IEEE Workshop on Advanced Robotics and its Social Impacts, 2005., IEEE, 2005, pp. 66-72.
T.L. Larsen, “Unmanned aerial vehicles for post disaster surveys,” Citeseer, 2010.
M. Onosato, et al., “Aerial robots for quick information gathering in USAR,” Proc. 2006 SICE-ICASE International Joint Conference, IEEE, 2006, pp. 3435-3438.
U. Iqbal, et al., “Selection of unmanned aerial system (uas) for disaster relief operations: A comparison,” Journal of Science International, 2015.
R. Austin, Unmanned aircraft systems: UAVs design, development and deployment, John Wiley & Sons, 2011.
X. Élie-dit-Cosaque, et al., “Design and drop test simulation of a helicopter skid landing gear with Abaqus/CAE,” Proc. SIMULIA Customer Conference, 2009, pp. 1-15.
S.N. Kumar, et al., “Design and Structural Analysis of Skid Landing Gear,” 2014.
D. Crist and L. Symes, Helicopter Landing Gear Design and Test Criteria Investigation, DTIC Document, 1981.
K. Shrotri, Composite skid landing gear design investigation, ProQuest, 2008.
R. Fazl-e-Umer, S. I. A. Shah and U. Iqbal, "Design of long range video and telemetry data transmission system for an UAV helicopter", Proceedings of 1st SMEP Applied Mechanical and Engineering Conference (AMEC-E), Lahore, Pakistan, November 14-16, 2014.
U. Iqbal, M. S. Sadiq and S. I. A. Shah, "Design, development and fabrication of airdrop mechanism for first aid kit drop in unmanned disaster relief helicopter",Proceedings of 3rd International Conference on Engineering and Emerging Technologies (ICEET), Lahore, Pakistan, April 07-08, 2016.
V. Hubka, Principles of engineering design, Elsevier, 2015.
D.D. Bedworth, et al., Computer-integrated design and manufacturing, McGraw-Hill, Inc., 1991.
G. Pahl and W. Beitz, Engineering design: a systematic approach, Springer Science & Business Media, 2013.
H. Howard and T. Gall, “Metals Handbook American Society for Metals,” Metals Park, OH, 1985.
F. Tooley, “Fiberglass,” ASM International, Engineered Materials Handbook., vol. 4, 1991, pp. 402-408.