ULPOWER 260i Aircraft Engine

ULPOWER 260i Aircraft engine

#4 stroke, 4 cylinder, horizontally opposed

#Dual (redundant) electronic spark ignition (variable timing)

#Electronic multipoint fuel injection (pressure and temperature compensated)

#Electronic RPM limiter

#Direct propeller drive

#5 bearing crankshaft with surface hardening treatment and additional large thrust bearing (ball bearing type)

#Single central camshaft

#Push rods, tappets and OHV (hydraulic compensators have not been used)

#Wet sump forced lubrication with integrated pressure regulator

#Ram air cooled cylinders and cylinder heads

#Integrated permanent magnet AC generator, external rectifier-regulator

#Electric starter

#Electric fuel pump and pressure regulator to eliminate vapor lock and facilitate starting even under adverse conditions