Bristol Taurus radial engine
GPTKB entity
Statements (24)
Predicate | Object |
---|---|
gptkbp:instanceOf |
piston engine
|
gptkbp:bore |
5.75 in
|
gptkbp:compressionRatio |
7.0:1
|
gptkbp:configuration |
two-row
|
gptkbp:coolingSystem |
air-cooled
|
gptkbp:countryOfOrigin |
gptkb:United_Kingdom
|
gptkbp:displacement |
2520 cubic inches
|
gptkbp:engineType |
piston engine
|
gptkbp:firstFlight |
1936
|
gptkbp:fuelType |
aviation gasoline
|
https://www.w3.org/2000/01/rdf-schema#label |
Bristol Taurus radial engine
|
gptkbp:manufacturer |
gptkb:Bristol_Aeroplane_Company
|
gptkbp:notableFeature |
sleeve valve design
|
gptkbp:numberOfEngines |
14
|
gptkbp:powerOutput |
up to 1,130 hp
|
gptkbp:predecessor |
gptkb:Bristol_Perseus
|
gptkbp:productionStartYear |
1936–1944
|
gptkbp:stroke |
6.5 in
|
gptkbp:successor |
gptkb:Bristol_Hercules
|
gptkbp:usedInAircraft |
gptkb:Bristol_Beaufort
gptkb:Bristol_Beaufighter_Mk_I |
gptkbp:bfsParent |
gptkb:Bristol_Beaufort
gptkb:Bristol_Beaufort_(historic) |
gptkbp:bfsLayer |
6
|