Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
114 mm
|
| gptkbp:compressionRatio |
4.9:1
|
| gptkbp:configuration |
V12
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:displacement |
20.3 L
|
| gptkbp:firstFlight |
1915
|
| gptkbp:fuelType |
petrol
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:notableEvent |
powered first non-stop transatlantic flight
used in Alcock and Brown's Vickers Vimy |
| gptkbp:numberBuilt |
4,681
|
| gptkbp:powerOutput |
225 hp
up to 360 hp |
| gptkbp:predecessor |
gptkb:Rolls-Royce_40/50_Silver_Ghost_engine
|
| gptkbp:productionStartYear |
1915–1928
|
| gptkbp:stroke |
165 mm
|
| gptkbp:successor |
gptkb:Rolls-Royce_Condor
|
| gptkbp:usedIn |
gptkb:Felixstowe_F.2A
gptkb:Handley_Page_O/400 gptkb:Vickers_Vimy gptkb:Airco_DH.4 |
| gptkbp:valvetrain |
gptkb:SOHC
|
| gptkbp:weight |
847 lb
|
| gptkbp:bfsParent |
gptkb:Rolls-Royce_engines
|
| gptkbp:bfsLayer |
8
|
| http://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Eagle (WWI)
|