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/aba9e5Additional 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