literature review on the future more electric aircraft (MEA) power system architecture and investigation of state of the art technologies for more-electric aircrafts
In an aircraft, the engine is the main energy source that supplies all the needed energy including the part used as proportion and the parts supplied to all the loads. The vision of optimizing aircraft performance, increasing reliability, reducing operating and maintenance costs as well as gas emiss...
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| Other Authors: | |
| Format: | Final Year Project (FYP) |
| Language: | English |
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2014
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| Online Access: | http://hdl.handle.net/10356/60815 |
| _version_ | 1811688058698858496 |
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| author | Hong, Yi |
| author2 | Wen Changyun |
| author_facet | Wen Changyun Hong, Yi |
| author_sort | Hong, Yi |
| collection | NTU |
| description | In an aircraft, the engine is the main energy source that supplies all the needed energy including the part used as proportion and the parts supplied to all the loads. The vision of optimizing aircraft performance, increasing reliability, reducing operating and maintenance costs as well as gas emission have push the development of aircraft industry toward the concept of more electric aircraft (MEA), and ultimately all electric aircraft. Recent improvement in the field of power electronic conversion systems, high density electric motors, power generation system, fault-tolerant design, electro-hydrostatic actuators and flight control systems have made the concept of MEA feasible.
In this paper, the importance and recent development of aircraft industry is introduced first. Then, the possible electrical system architecture including power generation and distribution systems as well state of art technologies of MEA is studied and compared with conventional aircraft. In order to optimizing the power generation of the aircraft generator, a simulation model of simple generator has been developed to help people in understanding the operation of generator and in the end facilitate people in the research and innovation of aircraft power system. |
| first_indexed | 2024-10-01T05:26:10Z |
| format | Final Year Project (FYP) |
| id | ntu-10356/60815 |
| institution | Nanyang Technological University |
| language | English |
| last_indexed | 2024-10-01T05:26:10Z |
| publishDate | 2014 |
| record_format | dspace |
| spelling | ntu-10356/608152023-07-07T16:41:13Z literature review on the future more electric aircraft (MEA) power system architecture and investigation of state of the art technologies for more-electric aircrafts Hong, Yi Wen Changyun School of Electrical and Electronic Engineering DRNTU::Engineering::Electrical and electronic engineering::Electric power In an aircraft, the engine is the main energy source that supplies all the needed energy including the part used as proportion and the parts supplied to all the loads. The vision of optimizing aircraft performance, increasing reliability, reducing operating and maintenance costs as well as gas emission have push the development of aircraft industry toward the concept of more electric aircraft (MEA), and ultimately all electric aircraft. Recent improvement in the field of power electronic conversion systems, high density electric motors, power generation system, fault-tolerant design, electro-hydrostatic actuators and flight control systems have made the concept of MEA feasible. In this paper, the importance and recent development of aircraft industry is introduced first. Then, the possible electrical system architecture including power generation and distribution systems as well state of art technologies of MEA is studied and compared with conventional aircraft. In order to optimizing the power generation of the aircraft generator, a simulation model of simple generator has been developed to help people in understanding the operation of generator and in the end facilitate people in the research and innovation of aircraft power system. Bachelor of Engineering 2014-05-30T08:12:18Z 2014-05-30T08:12:18Z 2014 2014 Final Year Project (FYP) http://hdl.handle.net/10356/60815 en Nanyang Technological University 53 application/pdf |
| spellingShingle | DRNTU::Engineering::Electrical and electronic engineering::Electric power Hong, Yi literature review on the future more electric aircraft (MEA) power system architecture and investigation of state of the art technologies for more-electric aircrafts |
| title | literature review on the future more electric aircraft (MEA) power system architecture and investigation of state of the art technologies for more-electric aircrafts |
| title_full | literature review on the future more electric aircraft (MEA) power system architecture and investigation of state of the art technologies for more-electric aircrafts |
| title_fullStr | literature review on the future more electric aircraft (MEA) power system architecture and investigation of state of the art technologies for more-electric aircrafts |
| title_full_unstemmed | literature review on the future more electric aircraft (MEA) power system architecture and investigation of state of the art technologies for more-electric aircrafts |
| title_short | literature review on the future more electric aircraft (MEA) power system architecture and investigation of state of the art technologies for more-electric aircrafts |
| title_sort | literature review on the future more electric aircraft mea power system architecture and investigation of state of the art technologies for more electric aircrafts |
| topic | DRNTU::Engineering::Electrical and electronic engineering::Electric power |
| url | http://hdl.handle.net/10356/60815 |
| work_keys_str_mv | AT hongyi literaturereviewonthefuturemoreelectricaircraftmeapowersystemarchitectureandinvestigationofstateofthearttechnologiesformoreelectricaircrafts |