Preliminary design of dual-system hybrid VTOL UAV for medical delivery purpose

2021 ◽  
Author(s):  
Fahmi Abdillah Sambodo ◽  
Willy Wahyanto ◽  
Marco Wijaya ◽  
Ghifari Hanif Mustofa ◽  
Muhammad Fikri Al-Fattah Isrinanto ◽  
...  
Keyword(s):  
Dual System ◽  
Preliminary Design ◽  
Vtol Uav ◽  
Medical Delivery

scholarly journals Preliminary Design Method and Prototype Testing of a Novel Rotors Retractable Hybrid VTOL UAV

IEEE Access ◽  
2021 ◽  
pp. 1-1
Author(s):  
Zijian Xiong ◽  
Yuanming Xu ◽  
Zhouyang Wang ◽  
Xuechao Pian ◽  
Yibing Wang
Keyword(s):  
Design Method ◽  
Preliminary Design ◽  
Vtol Uav ◽  
Prototype Testing

A Preliminary Design by Using Optimization for Tail-sitter VTOL UAV

2020 ◽  
Vol 30 (4) ◽  
Author(s):  
Luk Sawatdipon ◽  
Chinnapat Thipyopas, ◽  
Vis Sripawadkul ◽  
Tossapol Chayanon
Keyword(s):  
Preliminary Design ◽  
Vtol Uav

Preliminary design of a box-wing VTOL UAV

2019 ◽  
Vol 92 (5) ◽  
pp. 737-743
Author(s):  
Giuseppe Palaia ◽  
Vittorio Cipolla ◽  
Vincenzo Binante ◽  
Emanuele Rizzo
Keyword(s):  
Mechanical Design ◽  
Design Procedure ◽  
General Aviation ◽  
Preliminary Design ◽  
Content Type ◽  
Unmanned Air Vehicle ◽  
Vtol Uav ◽  
Air Vehicle ◽  
Aerodynamic Performances ◽  
Vtol Aircraft

Purpose This paper aims to present a preliminary study on a disruptive vertical take-off and landing (VTOL) configuration based on the best wing system concept by L. Prandtl. Design/methodology/approach A preliminary design has been addressed from several points of views: a conceptual design has been carried out thanks to in-house optimization tool; aerodynamic performances, propulsion design and mechanical design have been addressed to make the first prototype for preliminary vertical flight tests. Findings The study shows the feasibility of box-wing configuration for VTOL aircraft. Practical implications The work shows a general design procedure for box-wing unmanned air vehicle (UAV) configuration. The study of this configuration can be easily adopted in wider range, from UAV to general aviation. In the last category, it can be a promising configuration for the future of urban air mobility. Originality/value This work lays the foundation for studying and testing box-wing configuration for unmanned VTOL aircraft. The design procedure can be scaled to manned aircraft belonging to general aviation aircraft.

Preliminary design of vertical take-off and landing (VTOL) UAV with steerable vertical thrust effect

2010 ◽  
Author(s):  
Julian Tan Kok Ping ◽  
SauKeong Ban ◽  
ChingSeong Tan ◽  
Thomas Ting Shee Peng ◽  
Ng Chin Soon
Keyword(s):  
Preliminary Design ◽  
Vtol Uav

The Minnesota inverted-tee system: Parametric studies for preliminary design

PCI Journal ◽  
2012 ◽  
Vol 57 (2) ◽  
pp. 162-179
Author(s):  
Roberto Piccinin ◽  
Arturo E. Schultz
Keyword(s):  
Preliminary Design ◽  
Parametric Studies
Sign in / Sign up

Export Citation Format

Share Document