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Title
Author(s)
Citation
Spring to flight with clapping wings
Ang, Ziyuan
Ang, Z. (2014, March). Spring to flight with clapping
wings. Presented at Discover URECA @ NTU poster
exhibition and competition, Nanyang Technological
University, Singapore.
Date
2014
URL
http://hdl.handle.net/10220/24253
Rights
© 2014 The Author(s).
URECA
Undergraduate Research Experience on CAmpus
Category: 5
Student: Ang Ziyuan
School of Mechanical and Aerospace Engineering
FYP-URECA Project ID: MAE13001
Spring to Flight with Clapping Wings
Some insects adopt clap-and-fling wing maneuver during flight to generate more
aerodynamic thrust. However, such flapping flight is energetic costly, for wing
acceleration and deceleration. To fly efficiently, insects recover wing kinetic
energy by elastic energy storage. Conventional micro air vehicle (MAV), like the
Silverlit® i-Bird cannot store elastic energy using a revolute joint. This inspired our
flapping-wing micro air vehicle (MAV) to integrate flexural hinges to reduce
driving energy.
To illustrate the effect of the integrated spring on flapping flight, the MAV with
and without the springs are compared in terms of thrust per unit weight.
Clap and fling by insect
Silverlit® i-Bird (right)
Our Prototype MAV with elastic hinges
Flexural hinge and torsional representation
Clapping-wing MAV with elastic
hinges, produced more thrust than
that with revolute joint. However, it
has more room for improvement.
Maximum hover angle of prototype (left) and i-Bird (right)
Moment vs Angle, θ
Thrust to Weight Ratio
0.004
1
0.002
0.5
0
0
90
Prototype
140
Graph of hinge stiffness
I-Bird
Graph of thrust to weight ratio
Further tests can be done by varying the hinge stiffness to determine the optimal energy and weight
balance. This can be accomplished through the use of different materials and varying hinge lengths.
Project Title: Bio-inspired Flapping-wing Micro Air Vehicles
Supervisor: Asst Prof Lau Gih Keong
Collaborator: Mr Chin Yao Wei
www.ntu.edu.sg/ureca