Statements (31)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bore |
120 mm
|
| gptkbp:builtBy |
gptkb:Humber_Limited
gptkb:Gwynnes_Limited gptkb:Ruston_Proctor |
| gptkbp:configuration |
single-row rotary
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:France
|
| gptkbp:displacement |
16.3 L
|
| gptkbp:firstFlight |
1913
|
| gptkbp:fuelType |
petrol
|
| https://www.w3.org/2000/01/rdf-schema#label |
Clerget 9B rotary engine
|
| gptkbp:ignition |
dual magneto
|
| gptkbp:licenseBuiltIn |
gptkb:United_Kingdom
|
| gptkbp:manufacturer |
gptkb:Clerget-Blin
|
| gptkbp:notableFeature |
throttle control
|
| gptkbp:numberOfEngines |
9
|
| gptkbp:powerOutput |
130 hp
|
| gptkbp:stroke |
160 mm
|
| gptkbp:successor |
gptkb:Clerget_11B
|
| gptkbp:usedInAircraft |
gptkb:Nieuport_17
gptkb:Bristol_Scout gptkb:Avro_504 gptkb:Sopwith_Camel gptkb:Airco_DH.4 gptkb:Sopwith_Pup |
| gptkbp:usedInConflict |
gptkb:World_War_I
|
| gptkbp:valveConfiguration |
overhead valves
|
| gptkbp:weight |
168 kg
|
| gptkbp:bfsParent |
gptkb:Sopwith_Triplane
|
| gptkbp:bfsLayer |
6
|