Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bore |
4 in
|
| gptkbp:compressionRatio |
5.3:1
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:displacement |
867 cu in
|
| gptkbp:engineType |
V12 piston engine
|
| gptkbp:firstFlight |
1916
|
| gptkbp:fuelType |
carburetor
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Falcon
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:numberBuilt |
2,185
|
| gptkbp:powerOutput |
230-285 hp
|
| gptkbp:productionStartYear |
1916-1927
|
| gptkbp:stroke |
5.5 in
|
| gptkbp:successor |
gptkb:Rolls-Royce_Eagle
|
| gptkbp:usedInAircraft |
gptkb:Bristol_F.2_Fighter
gptkb:Vickers_Vimy gptkb:Airco_DH.4 |
| gptkbp:valvetrain |
gptkb:SOHC
|
| gptkbp:weight |
620 lb
|
| gptkbp:bfsParent |
gptkb:Bristol_F.2_Fighter
|
| gptkbp:bfsLayer |
6
|