cleo
Uploaded by
12 SLIDES
269 VUES
120LIKES

Progress Update: Solid-State Morphing Aircraft Development by MAE 435 Team

DESCRIPTION

This presentation outlines the ongoing development of a solid-state morphing aircraft, focusing on the feasibility of utilizing smart materials for ornithoptic flight in cruise conditions. Our interdisciplinary team aims to create a single-piece wing structure using only solid-state smart materials. The presentation covers aerodynamic wing designs, fuselage prototypes capable of a 6.5 lbf payload, and dynamic testing of macro fiber composites using advanced prototyping electronics like Arduino and Zduino. Future work will involve controller development and further testing.

1 / 12

Télécharger la présentation

Progress Update: Solid-State Morphing Aircraft Development by MAE 435 Team

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript

  1. Solid State Morphing Aircraft Team Members: Roger Bounthisane Elaine Gumapas Amber Cook Thoai Nguyen Jeremiah Silvis James Bird MAE 435 April 3, 2014 Status Update Presentation

  2. Objectives and Constraints • Prove the feasibility of smart materials in ornithoptic flight in cruise conditions • Use only solid state smart materials • Use a one piece wing surface c1 w2 Θ1 w1

  3. Group Structure MAE 435 April 3, 2014 Status Update Presentation

  4. Aerodynamics – Wing Designs MAE 435 April 3, 2014 Status Update Presentation

  5. FEA Complex Wing Design Testing various thicknesses in different locations of the wing • Different load cases examined: • Distributed load over the surface area • Distributed load along the edge • Pointed load at the end • Natural Frequency MAE 435 April 3, 2014 Status Update Presentation

  6. Structures - Fuselage Prototype • Capable of a 6.5lbf payload • Light weight design~ 38g • Does not need aerodynamic design • 1st iteration is designed with poster board. • Final design will be carbon fiber reinforced

  7. Structures – Four Bar Linkage MAE 435 April 3, 2014 Status Update Presentation

  8. Smart Materials MFC

  9. Macro Fiber Composite Testing LabView Program for Static and Dynamic MFC Testing

  10. Controls/Electronics • The Arduino UNO was used for prototyping, and the Zduino LEE is being fitted and prepared for the fuselage. • Bimorph signal generation, with fault safety, and frequency display.

  11. Future Work • Construct a wired controller • Perform MFC test with Arduino controller • Install Zduino LEE in fuselage

  12. MAE 435 April 3, 2014 Status Update Presentation

More Related