A Turbojet-Powered, High-Load Vertical Take-off and Landing Flight Platform

International Journal of Mechanical Engineering

© 2022 by SSRG - IJME Journal

Volume 9 Issue 3

Year of Publication : 2022

Authors : Wan Tang, Jiale Zheng, Xuerui Qi, Saixuan Chen

10.14445/23488360/IJME-V9I3P102

How to Cite?

Wan Tang, Jiale Zheng, Xuerui Qi, Saixuan Chen, "A Turbojet-Powered, High-Load Vertical Take-off and Landing Flight Platform," SSRG International Journal of Mechanical Engineering, vol. 9,  no. 3, pp. 15-23, 2022. Crossref, https://doi.org/10.14445/23488360/IJME-V9I3P102

Abstract:

In the paper, we propose a turbojet-powered vertical take-off and landing flight platform with high load performance for extreme terrain， which can be applied in the medical, marine, and military areas. The platform uses a matrix layout of four turbojet engines and a thrust vector control system to achieve smooth flight. The dynamics simulation model of the flight platform was also established to analyze the effect of airflow disturbance on its stability. We carried out the lightweight and streamlined shell design relying on the mainframe structure, which effectively applied the performance characteristics of the turbojet engine to the flight platform and ensured its high load performance and reliability. In addition, the flight platform is streamlined, integrated, and reliable and has a modular adjustable feature.

Keywords:

Turbojet powered, High load, Vertical take-off and Landing flight platform.

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