Pratt & Whitney R-1340

GPTKB entity

Properties (52)
Predicate Object
gptkbp:instanceOf aircraft engine
gptkbp:application military aircraft
civilian aircraft
gptkbp:compressionRatio 6.5:1
gptkbp:coolingSystem air-cooled
direct air cooling
gptkbp:displacement 1340 cubic inches
gptkbp:drivetrain overhead valves
gptkbp:engine sought after by collectors
horizontally opposed
popular among aviation enthusiasts
moderate vibration
influenced future engine designs
aircraft piston engine
replicas built for museums
gptkbp:engineConfiguration over 10,000 units
radial configuration
gptkbp:engineType multiple variants produced
gptkbp:exhibits featured in aviation exhibitions
gptkbp:firstFlight 1932
gptkbp:fuelType aviation gasoline
carbureted
magneto ignition
gptkbp:hasArea extensively tested during development
https://www.w3.org/2000/01/rdf-schema#label Pratt & Whitney R-1340
gptkbp:is_used_in gptkb:Douglas_DC-3
gptkb:Grumman_F4F_Wildcat
gptkb:Boeing_Stearman_PT-17
gptkbp:manufacturer gptkb:Pratt_&_Whitney
gptkbp:noise_level notable engine noise
gptkbp:notableUsers gptkb:Royal_Air_Force
gptkb:Royal_Canadian_Air_Force
gptkb:United_States_Army_Air_Forces
gptkb:United_States_Navy
gptkbp:operationalHistory widely_used_in_WWII
gptkbp:performances high reliability
restoration projects ongoing
detailed specifications available
good performance at altitude
relatively easy maintenance
technical documentation available
2700 RPM
gptkbp:powerOutput 600 horsepower
gptkbp:productionYears 1932-1945
gptkbp:propulsion fixed-pitch propeller
gptkbp:related_engine R-1340 family
R-1340 series
gptkbp:setting 9-cylinder
gptkbp:successor gptkb:Pratt_&_Whitney_R-985
gptkbp:torque high torque output
gptkbp:type radial engine
gptkbp:weight 450 pounds