Theoretical and Natural Science

- The Open Access Proceedings Series for Conferences


Theoretical and Natural Science

Vol. 13, 30 November 2023


Open Access | Article

Vertical takeoff and landing aircraft: Categories, applications, and technology

Derek Xiao Qin * 1
1 Conestoga High School

* Author to whom correspondence should be addressed.

Theoretical and Natural Science, Vol. 13, 126-129
Published 30 November 2023. © 2023 The Author(s). Published by EWA Publishing
This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
Citation Derek Xiao Qin. Vertical takeoff and landing aircraft: Categories, applications, and technology. TNS (2023) Vol. 13: 126-129. DOI: 10.54254/2753-8818/13/20240810.

Abstract

A Vertical Take-Off and Landing (VTOL) aircraft is an aircraft with the ability to take off and land vertically. The ability of removing the need for a runway allows VTOL aircraft to be used for applications that standard aircraft cannot be used for. These applications include military, firefighting, and transportation applications. For the purposes of this paper, helicopters will be considered to be VTOL aircraft, as they fit the general criteria and are among the first to be widely used. VTOL aircraft can be split into several categories, including hybrid VTOL aircraft, VTOL Unmanned Aerial Vehicles, and electric VTOL aircraft. These categories of VTOL aircraft are compared. Famous VTOL aircrafts like Osprey and Harrier are introduced. The technology behind VTOL aircraft is explained, and the ways in which VTOL aircraft can be made useful are reviewed. In addition, the prospect of VTOL aircraft has been made. This paper may offer a reference for the future works about VTOL.

Keywords

VTOL, Hybrid Aircraft, Helicopter

References

1. Doddi A 2016 Vertical Take-off and Landing (VTOL) American Institute of Aeronautics and Astronautics.

2. Doo J, Pavel M, Didey A, Hange C, Diller N, Tsairides M, Smith M, Bennet E, Bromfield M and Mooberry Jessie 2021 NASA Electric Vertical Takeoff and Landing(eVTOL) Aircraft Technology for Public Services - A White Paper.

3. Ducard G, Allenspach M 2021 Review of Designs and Flight control techniques of hybrid and convertible VTOL UAVs, Aerospace Science and Technology 118:107035.

4. Alaukik J, Amritanshu T, Ponnalgu R 2019 Modelling and Design of a Hybrid Aerial Vehicle Combining VTOL Capabilities With Fixed Wing Aircraft, 6th International Conference on Instrumentation, Control, and Automation (ICA), 47-51.

5. Oo W, Tun H, Naing Z, Moe W 2017 Design of Vertical Take-Off and Landing (VTOL) Aircraft System, International Journal of Science and Technology Research, 6:179-183.

6. Silva C, Johnson W, Antcliff K, Patterson M 2018 VTOL Urban Air Mobility Concept Vehicles for Technology Development, Aviation Technology, Integration, and Operations Conference.

7. Kuprikov M, Rabinskiy L 2018 Vertical Take-off and Landing Aircraft: Myth or Reality of Modern Aviation, Journal of Mechanical Engineering Research and Developments 41(4):46-52.

8. Stone R, Clarke G 2002 The T-Wing: A VTOL UAVA for Defense and Civilian Applications, Environmental Science.

9. Orhan I 2021 Estimation of helicopter emission and greenest helicopters for London, Aircraft Engineering and Aerospace Technology, 93(8):1333-1345.

10. Yang F, Pan Q, He T, Wu J, Gao Y 2018 A Study of structural design of flapping rotary wing aircraft IOP Conf. Series: Material Science and Engineering.

Data Availability

The datasets used and/or analyzed during the current study will be available from the authors upon reasonable request.

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Volume Title
Proceedings of the 3rd International Conference on Computing Innovation and Applied Physics
ISBN (Print)
978-1-83558-189-6
ISBN (Online)
978-1-83558-190-2
Published Date
30 November 2023
Series
Theoretical and Natural Science
ISSN (Print)
2753-8818
ISSN (Online)
2753-8826
DOI
10.54254/2753-8818/13/20240810
Copyright
30 November 2023
Open Access
This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited

Copyright © 2023 EWA Publishing. Unless Otherwise Stated