Published November 1, 2020 | Version v1
Journal article

Development and performance evaluation of a piezoceramic coated flapping wing

  • 1. Materials science division, CSIR-National Aerospace Laboratories, Bangalore (India)
  • 2. Centre for Nano Science and Engineering, Indian Institute of Science, Bangalore (India)

Description

Flapping wing applications require actuators that are light in weight and can produce large displacements. A piezoceramic coated flapping wing without any other amplification mechanism is developed for micro and nano aerial vehicles. The dragonfly wing shaped structure with the piezoceramic coating produced a lift of 0.99 mN which was 1.3 times the mass of the wing. The results obtained from the experiments to mimic the kinematic motions of the wing using the coated piezoceramic actuator are also reported. (paper)

Availability note (English)

Available from http://dx.doi.org/10.1088/1361-665X/aba9e5

Additional details

Identifiers

Publishing Information

Journal Title
Smart Materials and Structures (Print)
Journal Volume
29
Journal Issue
11
Journal Page Range
[9 p.]
ISSN
0964-1726

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
53045134
Subject category
S36: MATERIALS SCIENCE;
Descriptors DEI
ACTUATORS; EVALUATION; NANOTECHNOLOGY; PERFORMANCE; UNMANNED AERIAL VEHICLES
Descriptors DEC
AIRCRAFT