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
Link To Document :
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