A multipurpose modular drone with adjustable arms produced via the FDM additive manufacturing process

• Autorzy: Salvatore Brischetto , Alessandro Ciano , Carlo Giovanni Ferro
• Języki publikacji: EN

Abstrakty

EN

The present paper shows an innovative multirotor Unmanned Aerial Vehicle (UAV) which is able to easily and quickly change its configuration. In order to satisfy this feature, the principal structure is made of an universal plate, combined with a circular ring, to create a rail guide able to host the arms, in a variable number from 3 to 8, and the legs. The arms are adjustable and contain all the avionic and motor drivers to connect the main structure with each electric motor. The unique arm design, defined as all-in-one, allows classical single rotor configurations, double rotor configurations and amphibious configurations including inflatable elements positioned at the bottom of the arms. The proposed multi-rotor system is inexpensive because of the few universal pieces needed to compose the platform which allows the creation of a kit. This modular kit allows to have a modular drone with different configurations. Such configurations are distinguished among them for the number of arms, number of legs, number of rotors and motors, and landing capability. Another innovation feature is the introduction of the 3D printing technology to produce all the structural elements. In this manner, all the pieces are designed to be produced via the Fused Deposition Modelling (FDM) technology using desktop 3D printers. Therefore, an universal, dynamic and economic multi-rotor UAV has been developed.

Słowa kluczowe

EN

Unmanned Aerial Vehicle; multi-rotor; adjustablebox shaped arms; 3D printing; Fusion DepositionModelling

• Wydawca: De Gruyter Open
• Czasopismo: Curved and Layered Structures
• Rocznik: 2016
• Tom: 3
• Numer: 1

Daty

otrzymano

2016-05-20

zaakceptowano

2016-05-21

online

2016-07-05

Twórcy

autor

Salvatore Brischetto

• Department of Mechanical and Aerospace Engineering, Politecnico di Torino, Turin, Italy

autor

Alessandro Ciano

• Department of Mechanical and Aerospace Engineering, Politecnico di Torino, Turin, Italy

autor

Carlo Giovanni Ferro

• Department of Mechanical and Aerospace Engineering, Politecnico di Torino, Turin, Italy

Identyfikatory

DOI

10.1515/cls-2016-0016