The disclosure relates to a transitional aircraft. Specifically, the disclosure relates to a transitional aerial vehicle (AV), having a closed polygonal wing member allowing for, inter-alia; smaller dimensions (footprint) compared to AV with same lift/wing surface, higher payload capacity, vertical take-off and landing (VTOL), versatile flight modes (e.g., VTOL, hover, fixed wing cruising, side-to-side flight), effective work with rotors mounted with fixed longitudinal and transverse angle deflection in two arrays, longer flight time and distance, and the ability to self-stabilize landing on and taking off from uneven surfaces, with methods and modular systems for selectably releasing and protecting incorporated payload controllably inflated air-bags.
CLOSED POLYGONAL WING MEMBER AND USES THEREOF
GESCHLOSSENES POLYGONALES FLÜGELELEMENT UND VERWENDUNGEN DAVON
ÉLÉMENT D'AILE POLYGONALE FERMÉE ET SES UTILISATIONS
2024-08-07
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Min-# polygonal approximation of closed curves
IEEE | 2005
|Min-# Polygonal Approximation of Closed Curves
British Library Conference Proceedings | 2005
|