Design and development of synthetic jet actuator for underwater propulsion

The main objectives of this project were to design and develop two prototype synthetic jet actuators (SJAs) for use in underwater environments and capable of producing enough thrust to manoeuvre an underwater unmanned vehicle. One of the prototypes will be powered by an electric motor driving a cam...

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Main Author: Baird Matthew John
Other Authors: School of Mechanical and Aerospace Engineering
Format: Final Year Project
Language:English
Published: 2013
Subjects:
Online Access:http://hdl.handle.net/10356/54033
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Institution: Nanyang Technological University
Language: English
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spelling sg-ntu-dr.10356-540332023-03-04T19:35:47Z Design and development of synthetic jet actuator for underwater propulsion Baird Matthew John School of Mechanical and Aerospace Engineering Tang Hui DRNTU::Engineering::Mechanical engineering::Motors, engines and turbines The main objectives of this project were to design and develop two prototype synthetic jet actuators (SJAs) for use in underwater environments and capable of producing enough thrust to manoeuvre an underwater unmanned vehicle. One of the prototypes will be powered by an electric motor driving a cam and follower type arrangement to convert from rotary to linear movement; the other SJA is solenoid driven, using a linear solenoid to provide the diaphragm movement causing the thrust. This report details the methodology used to develop the designs for both of the SJAs as well as giving a background on some of the proposed tests which will be carried out on the final products. The test tank design and developments are also discussed. Tests were carried out on the completed motor driven SJA and the thrust delivered was calculated by taking a time average of the reaction forces from a load cell. The maximum force produced in preliminary testing was approximately 42N. The control systems for both the motor driven SJA and the solenoid driven SJA have been tested using an oscilloscope and sample components and allow the thrust to be altered through a microcontroller rather than a variable voltage source. The designs of the control systems and pasting methodology are covered in more detail. Finally some recommendations for further testing and improvements to both the design methodology and the design are given. Bachelor of Engineering (Mechanical Engineering) 2013-06-11T09:04:26Z 2013-06-11T09:04:26Z 2013 2013 Final Year Project (FYP) http://hdl.handle.net/10356/54033 en Nanyang Technological University 64 p. application/pdf
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic DRNTU::Engineering::Mechanical engineering::Motors, engines and turbines
spellingShingle DRNTU::Engineering::Mechanical engineering::Motors, engines and turbines
Baird Matthew John
Design and development of synthetic jet actuator for underwater propulsion
description The main objectives of this project were to design and develop two prototype synthetic jet actuators (SJAs) for use in underwater environments and capable of producing enough thrust to manoeuvre an underwater unmanned vehicle. One of the prototypes will be powered by an electric motor driving a cam and follower type arrangement to convert from rotary to linear movement; the other SJA is solenoid driven, using a linear solenoid to provide the diaphragm movement causing the thrust. This report details the methodology used to develop the designs for both of the SJAs as well as giving a background on some of the proposed tests which will be carried out on the final products. The test tank design and developments are also discussed. Tests were carried out on the completed motor driven SJA and the thrust delivered was calculated by taking a time average of the reaction forces from a load cell. The maximum force produced in preliminary testing was approximately 42N. The control systems for both the motor driven SJA and the solenoid driven SJA have been tested using an oscilloscope and sample components and allow the thrust to be altered through a microcontroller rather than a variable voltage source. The designs of the control systems and pasting methodology are covered in more detail. Finally some recommendations for further testing and improvements to both the design methodology and the design are given.
author2 School of Mechanical and Aerospace Engineering
author_facet School of Mechanical and Aerospace Engineering
Baird Matthew John
format Final Year Project
author Baird Matthew John
author_sort Baird Matthew John
title Design and development of synthetic jet actuator for underwater propulsion
title_short Design and development of synthetic jet actuator for underwater propulsion
title_full Design and development of synthetic jet actuator for underwater propulsion
title_fullStr Design and development of synthetic jet actuator for underwater propulsion
title_full_unstemmed Design and development of synthetic jet actuator for underwater propulsion
title_sort design and development of synthetic jet actuator for underwater propulsion
publishDate 2013
url http://hdl.handle.net/10356/54033
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