propulsion module
Wind Tunnel Testing and Aerodynamic Characterization of a QuadPlane Uncrewed Aircraft System
Electric Vertical Takeoff and Landing (eVTOL) vehicles will open new opportunities in aviation. This paper describes the design and wind tunnel analysis of an eVTOL uncrewed aircraft system (UAS) prototype with a traditional aircraft wing, tail, and puller motor along with four vertical thrust pusher motors. Vehicle design and construction are summarized. Dynamic thrust from propulsion modules is experimentally determined at different airspeeds over a large sweep of propeller angles of attack. Wind tunnel tests with the vehicle prototype cover a suite of hover, transition and cruise flight conditions. Net aerodynamic forces and moments are distinctly computed and compared for plane, quadrotor and hybrid flight modes. Coefficient-based models are developed. Polynomial curve fits accurately capture observed data over all test configurations. To our knowledge, the presented wind tunnel experimental analysis for a multi-mode eVTOL platform is novel. Increased drag and reduced dynamic thrust likely due to flow interactions will be important to address in future designs.
- North America > United States > Michigan > Washtenaw County > Ann Arbor (0.14)
- Asia > South Korea > Busan > Busan (0.04)
- North America > United States > Virginia > Montgomery County > Blacksburg (0.04)
- (4 more...)
- Transportation > Air (1.00)
- Automobiles & Trucks (1.00)
- Aerospace & Defense > Aircraft (1.00)
Reconfigurable Drone System for Transportation of Parcels With Variable Mass and Size
Schiano, Fabrizio, Kornatowski, Przemyslaw Mariusz, Cencetti, Leonardo, Floreano, Dario
Cargo drones are designed to carry payloads with predefined shape, size, and/or mass. This lack of flexibility requires a fleet of diverse drones tailored to specific cargo dimensions. Here we propose a new reconfigurable drone based on a modular design that adapts to different cargo shapes, sizes, and mass. We also propose a method for the automatic generation of drone configurations and suitable parameters for the flight controller. The parcel becomes the drone's body to which several individual propulsion modules are attached. We demonstrate the use of the reconfigurable hardware and the accompanying software by transporting parcels of different mass and sizes requiring various numbers and propulsion modules' positioning. The experiments are conducted indoors (with a motion capture system) and outdoors (with an RTK-GNSS sensor). The proposed design represents a cheaper and more versatile alternative to the solutions involving several drones for parcel transportation.
- Europe > Switzerland > Vaud > Lausanne (0.04)
- North America > United States > California > Los Angeles County > Long Beach (0.04)
- Aerospace & Defense > Aircraft (0.68)
- Transportation > Air (0.67)