A Requirements analysis methodology for turboelectric aircraft
Thesis: S.M., Massachusetts Institute of Technology, Department of Electrical Engineering and Computer Science, 2017.
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| Other Authors: | |
| Format: | Thesis |
| Language: | eng |
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Massachusetts Institute of Technology
2017
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| Online Access: | http://hdl.handle.net/1721.1/111912 |
| _version_ | 1826192073548627968 |
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| author | Dowdle, Aidan Patrick |
| author2 | Marija Ilić. |
| author_facet | Marija Ilić. Dowdle, Aidan Patrick |
| author_sort | Dowdle, Aidan Patrick |
| collection | MIT |
| description | Thesis: S.M., Massachusetts Institute of Technology, Department of Electrical Engineering and Computer Science, 2017. |
| first_indexed | 2024-09-23T09:05:51Z |
| format | Thesis |
| id | mit-1721.1/111912 |
| institution | Massachusetts Institute of Technology |
| language | eng |
| last_indexed | 2024-09-23T09:05:51Z |
| publishDate | 2017 |
| publisher | Massachusetts Institute of Technology |
| record_format | dspace |
| spelling | mit-1721.1/1119122019-04-10T09:06:54Z A Requirements analysis methodology for turboelectric aircraft Dowdle, Aidan Patrick Marija Ilić. Massachusetts Institute of Technology. Department of Electrical Engineering and Computer Science. Massachusetts Institute of Technology. Department of Electrical Engineering and Computer Science. Electrical Engineering and Computer Science. Thesis: S.M., Massachusetts Institute of Technology, Department of Electrical Engineering and Computer Science, 2017. Cataloged from PDF version of thesis. Includes bibliographical references (pages 81-82). The aviation industry today requires novel aircraft technology to provide for its rapidly growing demand. Of the many aircraft technologies being proposed, turboelectric is of particular interest for commercial-sized aircraft. Turboelectric propulsion enables novel airframe configurations, boundary layer ingestion, and distributed propulsion, each of which can reduce the amount of power and energy wasted during aircraft travel. In addition, it could reduce the aircraft noise. However, the drawbacks of switching to turboelectric propulsion are the added mass of the electrical components and the increased complexity in designing the system. Much research to date has focused on exploring the trade-offs between electrical vs. non-electrical propulsion systems in terms of weight. However, experience from terrestrial power systems suggests that the addition of electrical components into the propulsion system could have major impact in terms of dynamics. For instance, the electronic components could be used to meet thrust requirements faster than traditional turboprop engines could. On the other hand, large power deviations could potentially destabilize the electrical components. This thesis develops an analysis methodology to determine the requirements for a turboelectric aircraft prior to detailed design of the subsystems. by Aidan Patrick Dowdle. S.M. 2017-10-18T15:09:43Z 2017-10-18T15:09:43Z 2017 2017 Thesis http://hdl.handle.net/1721.1/111912 1005260429 eng MIT theses are protected by copyright. They may be viewed, downloaded, or printed from this source but further reproduction or distribution in any format is prohibited without written permission. http://dspace.mit.edu/handle/1721.1/7582 82 pages application/pdf Massachusetts Institute of Technology |
| spellingShingle | Electrical Engineering and Computer Science. Dowdle, Aidan Patrick A Requirements analysis methodology for turboelectric aircraft |
| title | A Requirements analysis methodology for turboelectric aircraft |
| title_full | A Requirements analysis methodology for turboelectric aircraft |
| title_fullStr | A Requirements analysis methodology for turboelectric aircraft |
| title_full_unstemmed | A Requirements analysis methodology for turboelectric aircraft |
| title_short | A Requirements analysis methodology for turboelectric aircraft |
| title_sort | requirements analysis methodology for turboelectric aircraft |
| topic | Electrical Engineering and Computer Science. |
| url | http://hdl.handle.net/1721.1/111912 |
| work_keys_str_mv | AT dowdleaidanpatrick arequirementsanalysismethodologyforturboelectricaircraft AT dowdleaidanpatrick requirementsanalysismethodologyforturboelectricaircraft |