Statements (34)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:displacement |
10.5 L
11.3 L |
| gptkbp:firstFlight |
1910s
|
| gptkbp:fuelType |
gptkb:gasoline
|
| gptkbp:manufacturer |
gptkb:Gnome_et_Rhône
|
| gptkbp:notableFeature |
lightweight design
reliable operation rotating crankcase and cylinders |
| gptkbp:notableModel |
gptkb:Le_Rhône_9J
gptkb:Le_Rhône_9C |
| gptkbp:numberOfEngines |
7
9 radial |
| gptkbp:operator |
gptkb:Royal_Flying_Corps
gptkb:French_Air_Force gptkb:Imperial_Russian_Air_Service United States Army Air Service |
| gptkbp:powerOutput |
110 hp
80 hp |
| gptkbp:successor |
gptkb:Gnome_Monosoupape
|
| gptkbp:usedDuring |
gptkb:World_War_I
|
| gptkbp:usedIn |
gptkb:aircraft
|
| gptkbp:usedInAircraft |
gptkb:Nieuport_17
gptkb:Avro_504 gptkb:Sopwith_Camel gptkb:Sopwith_Pup Morane-Saulnier N |
| gptkbp:bfsParent |
gptkb:TNCA_T-1
gptkb:Caudron_G.3 |
| gptkbp:bfsLayer |
8
|
| http://www.w3.org/2000/01/rdf-schema#label |
Le Rhône rotary engine
|