DocumentCode
540920
Title
Design for fault tolerance and predictive failures
Author
Wolmarans, J.J. ; Ferreira, J.A. ; Polinder, H. ; Josifovic, I. ; Clarenbach, D.
Author_Institution
Delft Univ. of Technol., Delft, Netherlands
fYear
2010
fDate
16-18 March 2010
Firstpage
1
Lastpage
6
Abstract
System integration and fault tolerance aims to help achieve high levels of availability and power density in aerospace applications. A 50kW integrated machine and drive with fault tolerance is described. For monitoring system health and diagnostics, an array of sensors is embedded. On state voltages and device currents are compared to ensure equal current sharing. By implementation of a power module using surface mount technology and double sided components a modular design is achieved. Key module parameters are constantly measured, through which faults can be detected and the ageing of a module may be quantified. Once a specific module has reached a predetermined age, the module may be removed from operation. The supporting system architecture will allow the remaining system to continue operation, therefore creating a fault tolerant system.
Keywords
aerospace instrumentation; electric drives; electric machines; fault tolerance; sensor arrays; surface mount technology; aerospace application; double sided component; fault tolerance design; fault tolerant system; integrated machine; power 50 kW; power density; power module; predictive failures; sensor array; surface mount technology; Current measurement; Fault tolerance; Fault tolerant systems; Semiconductor device measurement; Temperature measurement; Temperature sensors;
fLanguage
English
Publisher
ieee
Conference_Titel
Integrated Power Electronics Systems (CIPS), 2010 6th International Conference on
Conference_Location
Nuremberg
Print_ISBN
978-1-61284-814-3
Type
conf
Filename
5730631
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