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DC-bus power quality for aircraft power systems during generator fault conditions
DC-bus power quality for aircraft power systems during generator fault conditions
- Author(s): R. Todd and A.J. Forsyth
- DOI: 10.1049/iet-est.2010.0056
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- Author(s): R. Todd 1 and A.J. Forsyth 1
-
-
View affiliations
-
Affiliations:
1: School of Electrical and Electronic Engineering, University of Manchester, Manchester, UK
-
Affiliations:
1: School of Electrical and Electronic Engineering, University of Manchester, Manchester, UK
- Source:
Volume 1, Issue 3,
September 2011,
p.
126 – 135
DOI: 10.1049/iet-est.2010.0056 , Print ISSN 2042-9738, Online ISSN 2042-9746
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© The Institution of Engineering and Technology
Published
Higher-voltage, 540 V, aircraft DC-bus power quality is examined experimentally and by computer simulation during a short-circuit fault across the phase terminals of a 70 kW, five-phase, permanent magnet fault-tolerant generator. The DC-bus transients caused by the short-circuiting of the generator phases are seen to exceed the limits in MIL-STD-704F and a control algorithm is proposed for a supercapacitor-based energy storage device that mitigates the transients. The controller performance is illustrated by computer simulations for a range of bus switching scenarios.
Inspec keywords: aircraft power systems; fault tolerance; short-circuit currents; power supply quality; energy storage; permanent magnet generators; supercapacitors; power generation control; power generation faults
Other keywords:
Subjects: Aerospace power systems; Power supply quality and harmonics; Other energy storage; Control of electric power systems; d.c. machines; a.c. machines
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