Bristol Taurus radial engine
GPTKB entity
Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb: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 |
gptkb:piston_engine
|
| gptkbp:firstFlight |
1936
|
| gptkbp:fuelType |
aviation gasoline
|
| 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_(historic)
|
| gptkbp:bfsLayer |
6
|
| https://www.w3.org/2000/01/rdf-schema#label |
Bristol Taurus radial engine
|