Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:bore |
146 mm
|
| gptkbp:configuration |
14-cylinder
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
| gptkbp:displacement |
38.7 L
|
| gptkbp:engineType |
gptkb:piston_engine
|
| gptkbp:firstRun |
1939
|
| gptkbp:fuelType |
aviation gasoline
|
| gptkbp:manufacturer |
gptkb:Bristol_Aeroplane_Company
|
| gptkbp:notableFeature |
sleeve valve design
|
| gptkbp:numberBuilt |
over 57,400
|
| gptkbp:powerOutput |
1,290–1,735 hp
|
| gptkbp:productionStartYear |
1939–1950s
|
| gptkbp:stroke |
165 mm
|
| gptkbp:successor |
gptkb:Bristol_Centaurus
|
| gptkbp:supercharger |
single-stage, two-speed
|
| gptkbp:usedInAircraft |
gptkb:Vickers_Wellington
gptkb:aircraft gptkb:Short_Stirling gptkb:Bristol_Beaufighter gptkb:Armstrong_Whitworth_Albemarle |
| gptkbp:usedInConflict |
gptkb:World_War_II
|
| gptkbp:bfsParent |
gptkb:Aerospace_Bristol
gptkb:Bristol_Aeroplane_Company |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Bristol Hercules engine
|