Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
127 mm
|
| gptkbp:configuration |
V-12
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:displacement |
21.2 L
|
| gptkbp:engineType |
liquid-cooled V-12 piston engine
|
| gptkbp:firstRun |
1927
|
| gptkbp:fuelType |
gptkb:carburetor
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:notableFeature |
first Rolls-Royce engine to use pressurized cooling system
|
| gptkbp:powerOutput |
525–695 hp
|
| gptkbp:predecessor |
gptkb:Rolls-Royce_Eagle
|
| gptkbp:productionStartYear |
1927–1940s
|
| gptkbp:stroke |
140 mm
|
| gptkbp:successor |
gptkb:Rolls-Royce_Peregrine
|
| gptkbp:usedIn |
gptkb:Hawker_Fury
gptkb:Hawker_Hart gptkb:Heinkel_He_70 gptkb:Supermarine_Southampton Messerschmitt Bf 109 (early prototypes) |
| gptkbp:valvetrain |
DOHC, 4 valves per cylinder
|
| gptkbp:bfsParent |
gptkb:Hawker_Audax
|
| gptkbp:bfsLayer |
8
|
| http://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Kestrel V-12
|