Abstract
Wireless sensors have been widely suggested as a technology to extend the capability of Health and Usage Monitoring Systems (HUMS) on rotorcraft. Free from the constraints of hard wiring, wireless systems not only appear to offer a cost-effective solution, but in cases of instrumenting rotating or hard to reach parts, sometimes the only solution. Wireless data connections can be implemented using a range of mature technologies, however to be a truly wireless system, power cabling must be also be eliminated. This requires either local energy storage in a battery, energy harvesting (where power is generated from the ambient conditions of the sensor node), or a form of wireless power transfer. Of these solutions, only batteries can be considered mature. In this paper the power requirements of a wireless HUMS sensor node, designed to be mounted directly on the rotor head, are described and the possible power solutions considered. The very best energy-dense batteries currently available could power this node for many 100's of flight hours (for a reasonable battery volume) but it is unlikely these chemistries would be acceptable in the high stress rotating environment; battery technologies that are proven for high g environments would power this node for just a few 10's of flight hours. A vibration-powered generator is described which can produce up to 50mW average power during flight, potentially providing the 1000+ flight hours desirable for whole lifetime monitoring of rotor head parts.
Original language | English |
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Title of host publication | 40th European Rotorcraft Forum 2014 |
Publisher | Royal Aeronautical Society |
Pages | 1282-1292 |
Number of pages | 11 |
Volume | 2 |
ISBN (Print) | 9781510802568 |
Publication status | Published - 2014 |
Event | 40th European Rotorcraft Forum, ERF 2014 - Southampton, United Kingdom Duration: 2 Sept 2014 → 5 Sept 2014 |
Conference
Conference | 40th European Rotorcraft Forum, ERF 2014 |
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Country/Territory | United Kingdom |
City | Southampton |
Period | 2/09/14 → 5/09/14 |
Research Groups and Themes
- Engineering Mathematics Research Group