Design of a Single Phase Inverter for Aircraft Applications
Ozwin Dominic Dsouza1, Prajwal2, Arjun S3, Manjunath4, Tassmiya5
1Ozwin Dominic Dsouza, Assistant Professor in the Department of Electrical and Electronics Engineering at BMS Institute of Technology and Management.
2Prajwal Shetty, pursuing his Bachelor in Engineering in Electrical and Electronics Engineering Department at BMS Institute of Technology and Management Bengaluru.
3Arjun S, pursuing his Bachelor in Engineering in Electrical and Electronics Engineering Department at BMS Institute of Technology and Management Bengaluru.
4Manjunath pursuing his Bachelor in Engineering in Electrical and Electronics Engineering Department at BMS Institute of Technology and Management Besngaluru.
Manuscript received on 02 July 2019 | Revised Manuscript received on 09 July 2019 | Manuscript published on 30 July 2019 | PP: 2927-2929 | Volume-8 Issue-9, July 2019 | Retrieval Number: I8912078919/19©BEIESP | DOI: 10.35940/ijitee.I8912.078919
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© The Authors. Blue Eyes Intelligence Engineering and Sciences Publication (BEIESP). This is an open access article under the CC-BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/)
Abstract: This paper explains the design of inverter for aircraft application. Inverter is designed using the H-bridge connection of MOSFET. Gate voltage of the MOSFET is controlled by using arduino and mosfet driver connection. Designed inverter will support for 400Hz load. Inverted 400Hz voltage is displayed in 16*2 LCD display using the opto-coupler connection. This is the cost effective inverter design for high frequency application.
Keywords: PWM, MOSFET, H-Bridge, Opto-Coupler.
Scope of the Article: Low-power design