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http://arks.princeton.edu/ark:/88435/dsp015d86p266m
Title: | Design of a Folding-Wing Submersible Aircraft |
Authors: | Qin, Allen |
Advisors: | Stengel, Robert |
Department: | Mechanical and Aerospace Engineering |
Class Year: | 2016 |
Abstract: | A submersible aircraft has a large variety of envisioned applications: environmental research, search-and-rescue, surveillance, military defense, etc. Although there have been some success in submersible rotorcraft designs, no successful fixed-wing designs have been demonstrated. Follow-ing bio-inspiration from aquatic diving birds such as the cormorant, a folding wing mechanism is identified as a solution for the large hydrodynamic drag given by the large wingspan of conventional aircraft. The actuation mechanism utilizes a pair of four-bar linkages to constrain the motion of three primary joints to one, allowing for the full contraction and extension of the wing to be actuated by a single servomotor. The mechanism is supported within a detailed, original submersible fuselage design. Although the full manufacture of the design was not attempted, the folding wing mechanism and its integration with a submersible fuselage was conceptually validated by the physical demonstration of a positive result. |
Extent: | 64 pages |
URI: | http://arks.princeton.edu/ark:/88435/dsp015d86p266m |
Type of Material: | Princeton University Senior Theses |
Language: | en_US |
Appears in Collections: | Mechanical and Aerospace Engineering, 1924-2019 |
Files in This Item:
File | Size | Format | |
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Qin_Allen_Thesis.pdf | 13.61 MB | Adobe PDF | Request a copy |
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