LAPSE:2023.14258v1
Published Article

LAPSE:2023.14258v1
Electrical Launch Catapult and Landing Decelerator for Fixed-Wing Airborne Wind Energy Systems
March 1, 2023
Abstract
This paper presents a (pre)feasibility study of the rail-based ultra-short launch and landing system ElektRail for fixed-wing airborne wind energy systems, such as Ampyx Power. The ElektRail concept promises airborne mass reductions through the elimination of landing gear as well as decreased landing stresses and ground stability requirements, opening possibilities for improved aerodynamics through a single fuselage configuration. Initially designed for operating fixed-wing drones from open fields, the ElektRail concept had to be significantly shortened for application in an airborne wind energy (AWE) context. This shorter size is required due to the much more limited space available at AWE sites, especially on offshore platforms. Hence, a performance enhancement using the integration of a bungee launching and landing system (BLLS) was designed and a system dynamics model for the launch and landing was derived. The results demonstrated the possibility for the ElektRail to be shortened from 140 m to just 19.3 m for use with an optimised tethered aircraft with a mass of 317 kg. A system length below 20 m indicates that an enhanced ElektRail launch and landing concept could be viable for airborne wind energy operations, even with relatively low-tech bungee cord boosters. Linear motor drives with a long stator linear motor actuator could potentially shorten the system length further to just 15 m, as well as provide better control dynamics. An investigation into improved AWE net power outputs due to reduced airborne mass and aerodynamic improvements remains to be conducted.
This paper presents a (pre)feasibility study of the rail-based ultra-short launch and landing system ElektRail for fixed-wing airborne wind energy systems, such as Ampyx Power. The ElektRail concept promises airborne mass reductions through the elimination of landing gear as well as decreased landing stresses and ground stability requirements, opening possibilities for improved aerodynamics through a single fuselage configuration. Initially designed for operating fixed-wing drones from open fields, the ElektRail concept had to be significantly shortened for application in an airborne wind energy (AWE) context. This shorter size is required due to the much more limited space available at AWE sites, especially on offshore platforms. Hence, a performance enhancement using the integration of a bungee launching and landing system (BLLS) was designed and a system dynamics model for the launch and landing was derived. The results demonstrated the possibility for the ElektRail to be shortened from 140 m to just 19.3 m for use with an optimised tethered aircraft with a mass of 317 kg. A system length below 20 m indicates that an enhanced ElektRail launch and landing concept could be viable for airborne wind energy operations, even with relatively low-tech bungee cord boosters. Linear motor drives with a long stator linear motor actuator could potentially shorten the system length further to just 15 m, as well as provide better control dynamics. An investigation into improved AWE net power outputs due to reduced airborne mass and aerodynamic improvements remains to be conducted.
Record ID
Keywords
acceleration phase, airborne wind energy, Ampyx Power, AWES, BLLS, deceleration phase, ElektRail, landing, launch, system dynamics, UAV
Subject
Suggested Citation
Müller JA, Elhashash MYMK, Gollnick V. Electrical Launch Catapult and Landing Decelerator for Fixed-Wing Airborne Wind Energy Systems. (2023). LAPSE:2023.14258v1
Author Affiliations
Müller JA: Institute of Air Transportation Systems (ILT), Hamburg University of Technology, 21079 Hamburg, Germany [ORCID]
Elhashash MYMK: Institute of Air Transportation Systems (ILT), Hamburg University of Technology, 21079 Hamburg, Germany [ORCID]
Gollnick V: Institute of Air Transportation Systems (ILT), Hamburg University of Technology, 21079 Hamburg, Germany [ORCID]
Elhashash MYMK: Institute of Air Transportation Systems (ILT), Hamburg University of Technology, 21079 Hamburg, Germany [ORCID]
Gollnick V: Institute of Air Transportation Systems (ILT), Hamburg University of Technology, 21079 Hamburg, Germany [ORCID]
Journal Name
Energies
Volume
15
Issue
7
First Page
2502
Year
2022
Publication Date
2022-03-29
ISSN
1996-1073
Version Comments
Original Submission
Other Meta
PII: en15072502, Publication Type: Journal Article
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LAPSE:2023.14258v1
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https://doi.org/10.3390/en15072502
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Mar 1, 2023
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