Wright R-1600 engine

GPTKB entity

Properties (52)
Predicate Object
gptkbp:instanceOf aircraft engine
gptkbp:application military aircraft
gptkbp:bore 5.5 inches
gptkbp:compressionRatio 6.5:1
gptkbp:coolingSystem air-cooled
air-cooled radial
gptkbp:cylinderCount 14 cylinders
gptkbp:displacement 1,600 cubic inches
gptkbp:drivetrain pushrod actuated
gptkbp:engine innovative design features
single-speed supercharger
advanced technology for its time
radial layout
legacy in military aviation
Wright_design
gptkbp:engineConfiguration horizontally opposed
produced in large numbers
gptkbp:engineType multiple variants available
gptkbp:firstFlight 1940
gptkbp:fuel_capacity fuel consumption of 0.5 pounds per horsepower per hour
gptkbp:fuelType aviation gasoline
dual ignition
gptkbp:hasArea extensively tested
certified_by_FAA
https://www.w3.org/2000/01/rdf-schema#label Wright R-1600 engine
gptkbp:influence influenced future engine designs
gptkbp:is_used_in gptkb:Boeing_B-17_Flying_Fortress
gptkb:Douglas_A-26_Invader
gptkb:Lockheed_P-38_Lightning
gptkbp:manufacturer gptkb:Wright_Aeronautical_Corporation
gptkbp:maximum_speed maximum RPM of 2,700
gptkbp:notableUsers gptkb:United_States_Army_Air_Forces
gptkb:United_States_Navy
gptkbp:operationalHistory significant in aviation history
gptkbp:performances high performance
high reliability
long lifespan
detailed specifications available
moderate maintenance
characteristics of reliability and power
popular among military aircraft manufacturers
gptkbp:powerOutput 1,600 horsepower
gptkbp:productionYears 1940-1945
gptkbp:propulsion thrust of 1,600 pounds
gptkbp:related_engine gptkb:Wright_R-1600_series
gptkb:Wright_R-1600_family
gptkbp:stroke 6.0 inches
gptkbp:successor gptkb:Wright_R-1820_engine
gptkbp:torque high torque
gptkbp:type radial engine
gptkbp:updates upgraded versions developed
gptkbp:weight 1,200 pounds