Journal of Textile Science and Technology

Journal of Textile Science and Technology

Experimental Development of Tactical Aerostat Patching Scheme

Document Type : Research/ Original/ Regular Article

Authors
1 Assistant Professor, Space Transportation Research Institute, Iranian Space Research Center, Tehran, Iran
2 Researcher, Space Transportation Research Institute, Iranian Space Research Center, Tehran, Iran
Abstract
In an aerostat, the connection of the balloon to the ground is made through a rope called a tether, which is connected to the balloon body through several patchings. Patching plays a significant role in load-bearing and transferring the load to the balloon’s hull. Due to the high complexity stress analysis on patching, this study focuses on the development of its design through testing and analyzing of the results. In the first phase, to save time and cost, small-sized samples were prepared. By making changes to the way the ropes were connected, the type of fabric used, and the arrangement of patching, the initial design of the patching was ultimately achieved. After confirming the design in small samples, in the second phase, the patching was constructed in the actual size, and the effects of various factors on its strength were investigated. Then, by changing the way the patching fabric was connected to the base fabric and achieving an appropriate strength, the final patching design was completed. The last phase was evaluated using the actual fabric used in the balloon’s body. The tests performed in the final phase showed that the designed patching has the capability to withstand loads exceeding 8200 N and can bear the applied load with appropriate safety factor.
Keywords

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[1] Sharma, N., Sehgal, R., Pant, R. S., Design fabrication and deployment of a tethered aerostat system for aerial surveillance, National Level Conference on Advances in Aerial/Road Vehicle and its Application, 2014.
[2] Bilaye, P., Gawande, V., Desai, U., Low cost wireless internet access for rural areas using tethered aerostats, Third international Conference on Industrial and Information Systems, 2008.
[3] Dusane, C. R., Wani, A. V., Pant, R. S., An elevated balloon-kite hybrid platform for surveillance, 23rd AIAA Lighter-Than-Air Systems Technology Conference, 2017.
[4] tcomlp.com/image-tcom-operational-class-aerostat-systems-28m/
[5] Krausman, J. A., Petersen, S. T., The 22M class aerostat: increased capabilities for the small tethered aerostat surveillence system, 11th AIAA aviation technology, integration, and operation (ATIO) conference, 2011.
[6] revijahak.hr/2022/07/08/amerika-ima-novo-oruzje-za-rusiju-i-kinu-u-pripremi-su-baloni-koje-lete-na-velikim-visinama/
[7] Europian Aviatoin Safety Agency, Easy Access Rules for Tethered Gas Balloons (CS-31TGB) – 2018.
[8] Grant, E. C., Leland, M., Fundamentals of Aircraft and Airship Design. AIAA education series, 2013.
[9] Khoury, G. A., Gillett, J. D., Airship technology, Cambridge university press, 2012.
[10] Sarkheil, S., Jangi, A., Jafarian, A., Haghighat, V., Abbasi, A., Design, fabrication and operation of aerostat fabric permeability test device, The 30th annual international conference of Iranian society of mechanical engineers, ISME, 2022.
[11] Singha, K., A review on coating & lamination in textiles: processes and applications. American Journal of Polymer Science., 2, 39-49, 2012.
[12] Zhai, H., Euler, A., Material challenges for lighter-than-air systems in high altitude applications, AIAA 5th ATIO and16th Lighter-Than-Air Sys Tech. and Balloon Systems Conferences, 2005.
[13] Jangi, A., Sarkheil, S., Haghighat, V., Jafarian, A., Preparation and development of composite multi-layer fabric for airship/ aerostat, 13th national textile engineering conference, 2023.
[14] Chen, J., Chen, W., Central crack tearing testing of laminated fabric Uretek3216LV under uniaxial and biaxial static tensile loads. Journal of Materials in Civil Engineering., 28, 1-14, 2016.
[15] Reinhardt, H.W., On the biaxial testing and strength of coated fabrics. Experimental Mechanics., 16, 71-74, 1976.
[16] Meng, J., Lv, M., Qu, Z. and Li, P., Mechanical properties and strength criteria of fabric membrane for the stratospheric airship envelope. Applied Composite Materials., 24, 77-95, 2017.
[17] Yingying, Z., Xiaoguang, S., Qilin, Z., Henglin, L.V., Fracture failure analysis and strength criterion for PTFE-coated woven fabrics. Journal of Composite Materials., 49, 1409-1421, 2015.
[18] Mazrouei, Z., Khoddami, A., A review on superhydrophobicity: a characteristic property of textiles. Journal of Textile Science and Technology.,  3, 23-38, 2013.
[19] Keshe Farahani, M., Moghassem, A. R., Gohari, S. Z., Numerical simulation in plain woven fabrics. Journal of Textile Science and Technology.,  3, 61-68, 2013.
[20] Torabi, P., Abghari, M. J., Bidoki, S. M., Owlia, E., Evaluation of strain and deformation of the surface of woven fabrics using image correlation method. Journal of Textile Science and Technology., 11, 26-40, 2023.
[21] Myers, P. F., Vorachek, J. J., Definition of Tethered Balloon Systems. Goodyear Aerospace Corp Akron Oh, 1971.
[22] Bajoria, A., Mahto, N. K., Boppana, C. K., Design of a tethered aerostat system for animal and bird hazard mitigation, First International Conference on Recent Advances in Aerospace Engineering (ICRAAE), 2017.
[23] Jafarian, A., Sarkheil, S., Haghighat, V., Aerodynamic simulation of a tactical aerostat and evaluating the longitudinal static coefficients, Journal of space science, technology & applications.,  2, 73-83, 2022.
[24] Bagare, S. V., Joshi, A., Pant, R. S., A Methodology for Sizing of a Mini-Aerostat System, AIAA AVIATION 2021 FORUM, 2021.
[25] Jafarian, A., Sarkheil, S., Haghighat, V., Development of the conceptual design algurithm for tactical aerostats, Journal of solids and fluid mechanics., 13, 103-120, 2023.
 [26] Hunt, J. D., Structural Analysis of Aerostat Flexible Structure by the Finite-Element Method. Journal of Aircraft., 19, 674-678, 1982.
[27] Kumar, A., Sati, S. C., Ghosh, A. K., Design, Testing and Realization of a Medium Size Aerostat Envelope., Defense Science Journal., 66, 93-99, 2016.

  • Receive Date 18 December 2023
  • Revise Date 09 October 2024
  • Accept Date 10 November 2024