| dc.description.abstract | Flapping wing micro air vehicles (MAV) have broad applications such as exploration
in hazardous environment, reconnaissance, search and rescue. Ionic polymer metal
composites (IPMC) have emerged as a promising material in actuators and sensors
for use in flapping wing of MAVs. Though IPMC satifis es most of the criteria needed
for bio-inspired design, achieving high stiffness, actuation force, frequency and
flapping angle remains a challenge. The main objective of this thesis is to study the
various factors which influence the actuation performance of IPMC by mathematical
modelling, optimize design parameters for fabrication of high performing IPMC,
design an actuator-sensor array of IPMCs and fabrication of hybrid IPMC-polymer
structure as dragon y scale flapping wing of micro air vehicles. The dynamic mathematical
modelling of IPMC is carried out by variational principle using the Buechler
and Leo model and the performance of model actuators is studied. The structural
modelling of nanocomposite-based IPMC has been carried out to study the e ect of
inherent properties of the materials used in IPMC fabrication. The studies reveal that
the nanocomposite-based IPMC, IPMNC-RuO2/Na on and IPMNC-LbL CNC having
low thickness and high Youngs modulus can be actuated for higher deflection at
typical flapping frequencies (40-47 Hz). The structural modelling of unencapsulated
IPMCs (u-IPMC) intended for use under dry and humid environment is carried out for
optimization of design parameters for retention of water and to study the influence of
water activity on the actuation. IPMC designed with Na on having equivalent weight
900-1100, preheated at 30 C and sodium cation is more promising for optimum retention
of water and actuation. For operation in these environments, the actuation
parameters can be tuned to the desirable level by changing the water activity and
temperature of the user environment. For the design of dragon
y size flapping wing, the flexural stiffness of IPMC should be comparable to that of the actual insect wing
for proper flapping motion at higher flapping angle and deflection. Therefore, structural
modelling of dragon y scale IPMC is carried out. The IPMC actuator [IPMNCRuO
2/Na on with thickness 450 m (Na on 400 m and both electrodes 50 m ),
resonant frequency 31.5 Hz, Youngs modulus 2 GPa, mass 378 mg] modelled in
dragon y species, Sympetrum Frequens, shows better flapping and actuation than the
other insect scale actuators. In structural design of insect scale flapping wing, the
attachment of wing on the IPMC actuator as an array of actuator-sensor may lead
to self-powered flapping. The influence of attachment of wing on the actuator on the
actuation force and frequency to lift and flap the attached wing is studied. High frequency
(20 Hz) actuator (170 mg semi wet) with an attached mass equivalent to the
wing mass, produced higher actuation force, with reasonable frequency and deflection.
The studies on the dragon y scale flapping wing fabricated with IPMC-cyclic ole n
copolymer (COC) membrane based hybrid structure and the performance of various
wing confi gurations reveal that high frequency IPMC actuator fi tted with the high
modulus COC membrane with two-vein confi guration (leading edge and centre of the
wing) is the more promising structure as dragon y scale flapping wing. In conclusion,
with the analysis and design presented in this thesis, the optimized design and material
parameters of IPMC can be exploited for increased actuation performance at
the dragon y (Sympetrum Frequens) insect size. The high frequency IPMC can act
as flapping wing with capabilities of a sensor. The hybrid structure comprising high
frequency IPMC actuator fitted with the high modulus COC polymer membrane is a
promising flapping wing. The output voltage of IPMC wing could indicate the level of
actuation performance of the wing at different conditions such as change in temperature,
humidity or water content. Moreover, the actuator-sensor array can also help to
predict the environmental conditions and also used as an input for control algorithms. | en_US |
