Le Rhône 9‑cylinder rotary engine family
E466942
aircraft piston engine
aircraft piston engine family
air‑cooled aircraft engine
rotary aircraft engine
The Le Rhône 9‑cylinder rotary engine family was a widely used series of early 20th-century air-cooled aircraft engines that powered many Allied and Central Powers fighter and reconnaissance planes during World War I.
Observed surface forms (4)
| Surface form | Occurrences |
|---|---|
| Oberursel U.0 rotary engine | 1 |
| Oberursel UR.II rotary engine | 1 |
| Le Rhône 9C | 0 |
| Le Rhône 9J | 0 |
Statements (45)
| Predicate | Object |
|---|---|
| instanceOf |
aircraft piston engine
ⓘ
aircraft piston engine ⓘ aircraft piston engine family ⓘ air‑cooled aircraft engine ⓘ rotary aircraft engine ⓘ |
| application |
military aviation
ⓘ
training aircraft ⓘ |
| bore | 105 mm ⓘ |
| coolingSystem | air‑cooled ⓘ |
| countryOfOrigin | France ⓘ |
| cylinderConfiguration | single‑row rotary ⓘ |
| displacement | 11.3 L ⓘ |
| era | World War I NERFINISHED ⓘ |
| family | Le Rhône 9‑cylinder rotary engine family NERFINISHED ⓘ |
| firstFlightEra | pre‑World War I ⓘ |
| fuelType | gasoline ⓘ |
| ignitionSystem | magneto ignition ⓘ |
| licenseBuiltAs |
Oberursel U.0
NERFINISHED
ⓘ
Oberursel U.I NERFINISHED ⓘ |
| manufacturer | Société des Moteurs Le Rhône NERFINISHED ⓘ |
| notableFeature |
front‑mounted induction pipes
ⓘ
hollow crankshaft induction system ⓘ relatively low fuel consumption for a rotary engine ⓘ |
| notableVariant |
Le Rhône 9C
NERFINISHED
ⓘ
Le Rhône 9J NERFINISHED ⓘ |
| numberOfCylinders | 9 ⓘ |
| powerOutput |
110 hp
ⓘ
60 kW ⓘ 80 hp ⓘ 82 kW ⓘ |
| productionPeriod | 1910s ⓘ |
| stroke | 140 mm ⓘ |
| successor | Gnome‑Rhône radial engines NERFINISHED ⓘ |
| usedBy |
Allied Powers
NERFINISHED
ⓘ
Central Powers NERFINISHED ⓘ |
| usedInAircraft |
Fokker E.III (license‑built)
NERFINISHED
ⓘ
Nieuport 11 NERFINISHED ⓘ Nieuport 17 NERFINISHED ⓘ Sopwith Camel (license‑built variants) NERFINISHED ⓘ Sopwith Pup NERFINISHED ⓘ |
| usedInConflict | World War I ⓘ |
| usedInRole |
fighter aircraft propulsion
ⓘ
reconnaissance aircraft propulsion ⓘ |
| valveArrangement | two valves per cylinder ⓘ |
| valvetrain | single overhead camshaft ⓘ |
Referenced by (3)
Full triples — surface form annotated when it differs from this entity's canonical label.
this entity surface form:
Oberursel UR.II rotary engine
this entity surface form:
Oberursel U.0 rotary engine