Bristol Hercules engine

GPTKB entity

Properties (50)
Predicate Object
gptkbp:instanceOf aircraft engine
gptkbp:compressionRatio 6.5:1
gptkbp:coolingSystem air-cooled
gptkbp:cylinderCount 14 cylinders
gptkbp:displacement 36.5 L
36.5 liters
gptkbp:engine military aircraft
1,200 mm
military transport aircraft
bombers
transport aircraft
trainer aircraft
seaplanes
fighters
reconnaissance aircraft
naval aircraft
civil aircraft
passenger aircraft
flying boats
airliners
cargo_aircraft
gptkbp:engineConfiguration over 20,000 units
radial configuration
gptkbp:enginePower 2,000 hp
1,600 hp
gptkbp:engineType piston engine
gptkbp:firstFlight 1939
gptkbp:fuelType aviation gasoline
carbureted
magneto ignition
https://www.w3.org/2000/01/rdf-schema#label Bristol Hercules engine
gptkbp:is_used_in gptkb:Bristol_Beaufighter
gptkb:Bristol_Blenheim
Avro Lancaster
Short Sunderland
gptkbp:manufacturer gptkb:Bristol_Aeroplane_Company
gptkbp:notable_feature Hercules 1000
Hercules 1300
Hercules XVII
Hercules XX
Hercules_VI
gptkbp:origin gptkb:United_Kingdom
gptkbp:performances 2,500 rpm
gptkbp:powerOutput 1,600 to 2,000 hp
gptkbp:productionYears 1939-1960
gptkbp:setting two-row radial
gptkbp:successor gptkb:Bristol_Centaurus
gptkbp:torque 1,200 lb-ft
gptkbp:type radial engine
gptkbp:weight 1,200 lb