Rotax 914F
E694321
The Rotax 914F is a turbocharged four-cylinder aircraft engine widely used in light aircraft and unmanned aerial vehicles for its reliability and high power-to-weight ratio.
Statements (44)
| Predicate | Object |
|---|---|
| instanceOf |
aircraft engine
ⓘ
piston engine ⓘ |
| application |
light aircraft
ⓘ
ultralight aircraft ⓘ unmanned aerial vehicles ⓘ |
| bore | 84 mm ⓘ |
| compressionRatio | 7.0:1 ⓘ |
| configuration | four-cylinder ⓘ |
| coolant | water-glycol mixture ⓘ |
| coolingSystem |
air-cooled cylinders
ⓘ
liquid-cooled cylinder heads ⓘ |
| countryOfOrigin | Austria ⓘ |
| cylinderArrangement | horizontally opposed ⓘ |
| displacement | 1211 cc ⓘ |
| engineType | four-stroke ⓘ |
| family | Rotax 912/914 engine family NERFINISHED ⓘ |
| fuelSystem | carbureted ⓘ |
| fuelType |
AVGAS
ⓘ
MOGAS ⓘ |
| gearboxReductionRatio |
2.43:1
ⓘ
2.62:1 ⓘ |
| gearboxType | reduction gearbox ⓘ |
| ignitionSystem | dual electronic ignition ⓘ |
| induction | turbocharged ⓘ |
| manufacturer |
BRP-Rotax GmbH & Co KG
NERFINISHED
ⓘ
Rotax NERFINISHED ⓘ |
| marketSegment |
experimental aircraft
ⓘ
general aviation ⓘ light-sport aircraft ⓘ |
| maximumContinuousPower |
100 hp
ⓘ
73.5 kW ⓘ |
| maximumContinuousPowerRPM | 5500 rpm ⓘ |
| notableCharacteristic |
high power-to-weight ratio
ⓘ
high-altitude performance ⓘ reliability ⓘ |
| numberOfCylinders | 4 ⓘ |
| powerOutput |
115 hp
ⓘ
85 kW ⓘ |
| ratedPowerRPM | 5800 rpm ⓘ |
| relatedEngine |
Rotax 912ULS
NERFINISHED
ⓘ
Rotax 914 UL NERFINISHED ⓘ |
| stroke | 61 mm ⓘ |
| turbochargerControl | automatic wastegate control ⓘ |
| valvetrain | overhead camshaft ⓘ |
Referenced by (1)
Full triples — surface form annotated when it differs from this entity's canonical label.