dc.contributor.author |
Coetzer, Adél
|
|
dc.contributor.author |
Turner, Geoffrey R
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|
dc.contributor.author |
Mouton, T
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|
dc.date.accessioned |
2018-07-02T08:45:59Z |
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dc.date.available |
2018-07-02T08:45:59Z |
|
dc.date.issued |
2017-09 |
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dc.identifier.citation |
Coetzer, A., Turner, G.R. and Mouton, T. 2017. Power generation on-board aircraft using an air-powered turbine generator and battery interface system. 19th European Conference on Power Electronics and Applications (EPE'17 ECCE Europe), 11-14 September 2017, Warsaw, Poland |
en_US |
dc.identifier.isbn |
978-90-75815-27-6 |
|
dc.identifier.isbn |
978-1-5386-0530-1 |
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dc.identifier.uri |
https://ieeexplore.ieee.org/document/8098939/
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|
dc.identifier.uri |
DOI: 10.23919/EPE17ECCEEurope.2017.8098939
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|
dc.identifier.uri |
http://hdl.handle.net/10204/10287
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|
dc.description |
Copyright: 2017 IEEE. Due to copyright restrictions, the attached PDF file contains the accepted version of the published item. For access to the published paper, please consult the publisher's website. |
en_US |
dc.description.abstract |
The design and implementation of a prototype hybrid power generation system, consisting of a ram air turbine (RAT) generator and an energy storage unit, is presented. The system is intended as a mechanism to supply additional or emergency power on-board an aircraft. Here we present the design, manufacture and testing of a synchronous rectifier required to interface an asynchronous generator to a dc bus. The dc bus connects to a battery of electrochemical cells through a bidirectional dc-dc converter. The dc-dc converter functions to regulate the dc bus voltage by utilising a double control loop strategy with an inner current control loop and outer voltage control loop. The power delivered to the dc bus from the generator is controlled as a function of the battery voltage, dc bus current and generator shaft speed. The control strategy used by the prototype circuit is presented in this paper along with simulation and experimental results. |
en_US |
dc.language.iso |
en |
en_US |
dc.publisher |
IEEE |
en_US |
dc.relation.ispartofseries |
Worklist;21010 |
|
dc.subject |
Hybrid power integration |
en_US |
dc.subject |
Adjustable speed generation system |
en_US |
dc.subject |
Converter control |
en_US |
dc.subject |
AC machine |
en_US |
dc.subject |
Generator excitation system |
en_US |
dc.subject |
Airplane |
en_US |
dc.subject |
Batteries |
en_US |
dc.title |
Power generation on-board aircraft using an air-powered turbine generator and battery interface system |
en_US |
dc.type |
Conference Presentation |
en_US |
dc.identifier.apacitation |
Coetzer, A., Turner, G. R., & Mouton, T. (2017). Power generation on-board aircraft using an air-powered turbine generator and battery interface system. IEEE. http://hdl.handle.net/10204/10287 |
en_ZA |
dc.identifier.chicagocitation |
Coetzer, Adél, Geoffrey R Turner, and T Mouton. "Power generation on-board aircraft using an air-powered turbine generator and battery interface system." (2017): http://hdl.handle.net/10204/10287 |
en_ZA |
dc.identifier.vancouvercitation |
Coetzer A, Turner GR, Mouton T, Power generation on-board aircraft using an air-powered turbine generator and battery interface system; IEEE; 2017. http://hdl.handle.net/10204/10287 . |
en_ZA |
dc.identifier.ris |
TY - Conference Presentation
AU - Coetzer, Adél
AU - Turner, Geoffrey R
AU - Mouton, T
AB - The design and implementation of a prototype hybrid power generation system, consisting of a ram air turbine (RAT) generator and an energy storage unit, is presented. The system is intended as a mechanism to supply additional or emergency power on-board an aircraft. Here we present the design, manufacture and testing of a synchronous rectifier required to interface an asynchronous generator to a dc bus. The dc bus connects to a battery of electrochemical cells through a bidirectional dc-dc converter. The dc-dc converter functions to regulate the dc bus voltage by utilising a double control loop strategy with an inner current control loop and outer voltage control loop. The power delivered to the dc bus from the generator is controlled as a function of the battery voltage, dc bus current and generator shaft speed. The control strategy used by the prototype circuit is presented in this paper along with simulation and experimental results.
DA - 2017-09
DB - ResearchSpace
DP - CSIR
KW - Hybrid power integration
KW - Adjustable speed generation system
KW - Converter control
KW - AC machine
KW - Generator excitation system
KW - Airplane
KW - Batteries
LK - https://researchspace.csir.co.za
PY - 2017
SM - 978-90-75815-27-6
SM - 978-1-5386-0530-1
T1 - Power generation on-board aircraft using an air-powered turbine generator and battery interface system
TI - Power generation on-board aircraft using an air-powered turbine generator and battery interface system
UR - http://hdl.handle.net/10204/10287
ER -
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en_ZA |