Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
6.0 in
|
| gptkbp:compressionRatio |
6:1
|
| gptkbp:coolingSystem |
liquid-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:displacement |
36.7 litres
|
| gptkbp:engineType |
V-12 piston engine
|
| gptkbp:firstRun |
1939
|
| gptkbp:fuelType |
aviation gasoline
|
| gptkbp:manufacturer |
gptkb:Rolls-Royce_Limited
|
| gptkbp:powerOutput |
1,735 hp
|
| gptkbp:stroke |
6.6 in
|
| gptkbp:successor |
gptkb:Rolls-Royce_Griffon_57
|
| gptkbp:supercharger |
single-stage, two-speed
|
| gptkbp:usedInAircraft |
gptkb:aircraft
gptkb:Fairey_Firefly |
| gptkbp:weight |
1,980 lb
|
| gptkbp:bfsParent |
gptkb:Fairey_Firefly_FR.1
gptkb:Fairey_Firefly_TT.80 |
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
Rolls-Royce Griffon IIB
|