<abstract xmlns="http://www.w3.org/1999/xhtml">

<p>As the rotor configuration has the most impact on helicopter properties, the process of determination the assumptions for rotor design is a very important factor in the early stage of rotorcraft development. The following paper presents a mechanical analysis process used at the Institute of Aviation to quickly develop a coaxial rotor prototype applicable in ultra-light unmanned helicopter which has the potential for further improvement of its flight parameters. The article describes the rotor analysis process due to its feasibility based on commercially available solutions, the process of formulating assumptions for the entire structure, MES analysis of the rotor parts all leading to creation of the rotor prototype.</p>
</abstract>

As the rotor configuration has the most impact on helicopter properties, the process of determination the assumptions for rotor design is a very important factor in the early stage of rotorcraft development. The following paper presents a mechanical analysis process used at the Institute of Aviation to quickly develop a coaxial rotor prototype applicable in ultra-light unmanned helicopter which has the potential for further improvement of its flight parameters. The article describes the rotor analysis process due to its feasibility based on commercially available solutions, the process of formulating assumptions for the entire structure, MES analysis of the rotor parts all leading to creation of the rotor prototype.

Mechanical Analysis Process of a Coaxial Counter Rotor for Applications in Unmanned Ultra-Light Units

Transactions on Aerospace Research

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

As the rotor configuration has the most impact on helicopter properties, the process of determination the assumptions for rotor design is a very important...

Mechanical Analysis Process of a Coaxial Counter Rotor for Applications in Unmanned Ultra-Light Units

Published Online: Jul 25, 2019

Page range: 38 - 58

DOI: https://doi.org/10.2478/tar-2019-0009

Keywords
rotor analysis, coaxial rotor, ultra-light

© 2017 Copyright by Lukasiewicz Research Network – Institute of Aviation

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

Mechanical Analysis Process of a Coaxial Counter Rotor for Applications in Unmanned Ultra-Light Units

Published Online: Jul 25, 2019

Page range: 38 - 58

DOI: https://doi.org/10.2478/tar-2019-0009

Keywordsrotor analysis, coaxial rotor, ultra-light

© 2017 Copyright by Lukasiewicz Research Network – Institute of Aviation

This work is licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 3.0 License.

Keywords
rotor analysis, coaxial rotor, ultra-light