Folding Container Single Phase for Unmanned Aerial Vehicle Station
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Design and field test of a foldable wing unmanned aerial–underwater vehicle
Nov 14, 2023 · This paper presents the design and field test of a foldable wing unmanned aerial–underwater vehicle (UAUV). The vehicle can complete diving and air operations, and
Unmanned Aerial Vehicle Base Station (UAV-BS) Deployment
Nov 20, 2019 · Unmanned aerial vehicle (UAV) with flexible mobility and low cost has been a promising technology for wireless communication. Thus, it can be used for wireless data
Unmanned aerial vehicles: A review
Jan 1, 2023 · The lightweight Unmanned Aerial Vehicle (UAV) flight activities are constrained, particularly in the UAV range or activity span and perseverance, by the strategic
Distributed decision making for unmanned aerial vehicle
Dec 1, 2024 · The unsatisfactory energy density of the state-of-art batteries imposes constraints on the practical application of unmanned aerial vehicles (UAVs). Establishing a UAV airport
Design of a Foldable Multirotor for Rapid Deployment in
Apr 24, 2024 · Abstract. To cope with complex scenarios and unexpected situations, it is impor-tant to improve the portability and rapid deployment capability of unmanned aerial vehicles
Spray-on steady-state study of multi-rotor cleaning unmanned aerial
Jun 1, 2024 · Y Zheng et al. (2018) proposed that the downwash flow field generated by the rotors of a multi-rotor unmanned aerial vehicle (UAV) during operation has a significant impact on the
Aerodynamic design optimization of twice folding wing for
Abstract: The twice folding wing can effectively increase the aspect ratio of the wing of tube-launched UAV and improve the cruising efficiency of the UAV. However, the flat-angle rotation
Foldable unmanned aerial vehicle capable of being carried by single
The foldable unmanned aerial vehicle has the beneficial effects that flight is smooth and steady, reliability is high, the wing loads are reduced, running time is prolonged, the unfolding
WO/2019/080182 WING FOLDING MECHANISM FOR UNMANNED AERIAL VEHICLE
Sep 11, 2017 · The unmanned aerial vehicle can reduce its volume by folding the first folding wings (3) and the second folding wings (4), thereby reducing a space it occupies.
Aerodynamic Characteristics of Unmanned Aerial Vehicle
Apr 25, 2025 · To accurately capture the flowfield distribution of Z-shaped folding wings under different configurations, especially the airflow separation caused by the dihedral angles
Design and Simulation of Foldable Wing eVTOL UAV
Urban Air Mobility (UAM) has garnered significant global attention due to its potential to revolutionize transportation. The utilization of Electric Vertical Take-Off and Landing (eVTOL)
Design and field test of a foldable wing unmanned aerial–underwater vehicle
Nov 14, 2023 · The aquatic unmanned aerial vehicle (AquaUAV), a kind of vehicle that can operate both in the air and the water, has been regarded as a new breakthrough to broaden
Design of folded wing mechanism for Unmanned Aerial Vehicle (UAV)
Jan 1, 2022 · The main aim of this project is design of folded wing mechanism for small-UAV (<15 kg) and minimize storing and shipping space required. The paper gives review of design of
A Novel Folding Wireless Charging Station Design for Drones
Jun 26, 2024 · Unmanned aerial vehicles (UAV) have been used in many fields nowadays. In long-term applications, batteries need to be constantly changed by someone due to short
Design and Simulation of Foldable Wing eVTOL UAV
Aug 14, 2024 · As a new type of UAV technology, electric vertical take-off and landing Unmanned Aerial Vehicle (eVTOL UAV) has the advantages of vertical take-off and landing, vertical flight
Design of a Micro-Scale Deployable Unmanned Aerial
Feb 23, 2023 · The design of a micro-scale, autonomous, unmanned aerial vehicle, deployed from a cylindrical container is presented. The integration of elements unique to deployable aircraft,
Efficient charging station deployment in unmanned aerial vehicle
Apr 28, 2025 · Unmanned Aerial Vehicles (UAVs) are flexible autonomous systems that enable efficient data collection and task execution across diverse applications. However, their limited
FAQS 4
Can a foldable wing unmanned aerial–underwater vehicle egress water?
This paper presents the design and field test of a foldable wing unmanned aerial–underwater vehicle (UAUV). The vehicle can complete diving and air operations, and still have the ability of multiple trans‐medium water egress and ingress under the condition of carrying mission load during a single flight.
What is folded wing mechanism for small UAV?
Most of the UAV are open wing mechanism that causes problem to transport UAVs to other places due to require large space. The main aim of this project is design of folded wing mechanism for small-UAV (<15 kg) and minimize storing and shipping space required.
What is electric vertical take-off and landing UAV?
As a new type of UAV technology, electric vertical take-off and landing Unmanned Aerial Vehicle (eVTOL UAV) has the advantages of vertical take-off and landing, vertical flight and portability, which is widely used in military, civil and commercial fields.
What is folding wing mechanism for small-UAV (15 kg)?
The paper gives review of design of folded wing mechanism for small-UAV (<15 kg) and motion analysis results for mechanism. Role of mechanism as to fold the wings in idle position manually and automatically open the wings when released from launcher and hold the wings by spring force while travelling.
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