Publications
Detailed Information
Design for Flapping Wing Micro Vehicle Using 6-Bar Linkage Mechanism : 6절 링크를 이용한 날갯짓 초소형 비행체 설계
Cited 0 time in
Web of Science
Cited 0 time in Scopus
- Authors
- Advisor
- 신상준
- Major
- 공과대학 기계항공공학부
- Issue Date
- 2016-02
- Publisher
- 서울대학교 대학원
- Keywords
- Flapping wing ; Multi-body dynamic analysis ; Six-bar linkage
- Description
- 학위논문 (석사)-- 서울대학교 대학원 : 기계항공공학부, 2016. 2. 신상준.
- Abstract
- Recently, there occurs rise and growth of the research on the flapping wing vehicles
by mimicking the biological motion. Its result is so-called the Flapping Micro Aerial
Vehicle (FWMAV). In this thesis, design requirements for FWMAV were established
by using an analytical tool and unsteady blade element theory (UBET). Based on the
present FWMAV design requirements, flapping wing mechanism using a six-bar
linkage was devised. Moreover, the present mechanisms were analyzed by using the
flexible multi-body dynamic analysis to ensure its structural robustness. By
completing such procedure, behavior of the present mechanism was estimated. Then,
detail design was conducted. Currently, structural analysis regarding the present
mechanism was conducted under the flapping operation in vacuum. And the
resulting von-Misses stresses in the linkage were designed to be smaller than the
yield stress of the chosen material. After that, detail design and experiment of the
present FWMAV were conducted for validating the performance, such as
aerodynamic force, flapping frequency and flapping amplitude.
- Language
- English
- Files in This Item:
Item View & Download Count
Items in S-Space are protected by copyright, with all rights reserved, unless otherwise indicated.