First 4 Concept Designs:
4 Concepts were initially considered:
-A: Included 4 Rotors (Quadcopter) + Conventional aircraft design
-B: Included 3 Rotors (Tricopter) + Conventional Aircraft
-C: Included 3 Rotors (Tricopter) + Aircraft with Tail rotor as vector thrust
-D: Aircraft design with ducted fans in the wings
Chosen Design:
-From the weight utility function attached in the files folder (File Name), the Concept C was selected as the preliminary design concept.
Concept idea by:
Brian C. Kovarik
INITIAL CAD DESIGN:
-Modeled in PTC Creo Parametrics II by:
Adria Serra Moral
Forward Thrust Aircraft Configuration:
Vertical Thrust Tricopter Configuration
FINAL DESIGN:
Due to stability reasons, the team decided to go back and select concept B which, as shown below, includes a conventional aircraft configuration with an aft tail.
FINAL CAD DESIGN:
-Modeled in PTC Creo Parametrics II by:
Adria Serra Moral
Forward Thrust Aircraft Configuration:
Vertical Thrust Tricopter Configuration
Interior Design