RCV 35cc UAV JP8 engine under dynamometer test, from http://www.rcvengines.com
RCV engine information from http://rcvengines.com/rcv_modelhome.htm
capacity in cc | power output in kWatts | kW / kg | J/ccfam |
---|---|---|---|
10 | 0.670 at 5,400 rpm | 1.175 | 0.744 |
15 | 1.120 at 5,400 rpm | 1.427 | 0.830 |
20 | 1.340 at 5,400 rpm | 1.34 | 0.744 |
Notes
from http://www.sae.org/aeromag/techupdate/09-2006/2-26-8-5.pdf
An engine prototype displayed at the AUVSI Conference 2008 in San Diego.
The RCV engine is particularly suited to UAV applications because it runs extremely well on heavy fuels, typically generating the same power levels that it does on gasoline. The excellent JP5/JP8 running characteristics, are due to the compact combustion chamber and high internal turbulence levels, generated by the large squish area, sharp valve edges and rotating cylinder.
RCV have developed and patented a reliable cold start system, for use with heavy fuels.
Benefits include:
These engines are designed to give low Brake Specific Fuel Consumption (BSFC) at part throttle:
Observed on general RCV engines | Fixed valve timing and compression engine (JP-8) | Variable valve timing and compression engine (JP-8) | Typical conventional automotive |
---|---|---|---|
82 KW / litre | 82 KW / litre | 82 KW / litre | 75 KW / litre |
630 g / KW | < 350 g / KW | < 400 g / KW | 500 - 600 g / KW |
290 g / KWhr | 270 g / KWhr | 270 g / KWhr | 300 g / KWhr |
396 g / KWhr | 331 g / KWhr | 440 g / KWhr |