gptkbp:instanceOf
|
piston engine
|
gptkbp:bore
|
4.5 in (114 mm)
|
gptkbp:configuration
|
V12
|
gptkbp:coolingSystem
|
liquid-cooled
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
gptkbp:displacement
|
20.3 L (1,239 cu in)
|
gptkbp:engineType
|
V12 liquid-cooled piston engine
|
gptkbp:firstFlight
|
1915
|
gptkbp:fuelType
|
petrol
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Eagle engine
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce_Limited
|
gptkbp:notableEvent
|
powered the first non-stop transatlantic flight (Alcock and Brown, 1919)
|
gptkbp:notableUser
|
gptkb:Royal_Air_Force
gptkb:Royal_Naval_Air_Service
|
gptkbp:numberBuilt
|
4,681
|
gptkbp:powerOutput
|
225 hp (initial version)
up to 360 hp (later versions)
|
gptkbp:predecessor
|
gptkb:Rolls-Royce_40/50_Silver_Ghost_engine
|
gptkbp:productionStartYear
|
1915–1928
|
gptkbp:stroke
|
6.5 in (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:bfsParent
|
gptkb:Sir_Henry_Royce
gptkb:Henry_Royce
|
gptkbp:bfsLayer
|
6
|