Wright R-3350 engine

GPTKB entity

Properties (69)
Predicate Object
gptkbp:instanceOf aircraft engine
gptkbp:application commercial aircraft
military aircraft
gptkbp:compressionRatio 6.5:1
gptkbp:controls automatic propeller control
gptkbp:coolingSystem air-cooled
cylinder_head_cooling
gptkbp:displacement 3,350 cubic inches
gptkbp:drivetrain pushrod actuated
gptkbp:engine horizontally opposed
moderate vibration
two-speed supercharger
cradle_mount
gptkbp:engineType gptkb:R-3350-26
R-3350-32
R-3350-75
R-3350-100
R-3350-105
R-3350-115
R-3350-175
R-3350-195
R-3350-200
R-3350-57
R-3350-23
R-3350-89
R-3350-95
R-3350-99
R-3350-110
R-3350-120
R-3350-125
R-3350-130
R-3350-135
R-3350-140
R-3350-145
R-3350-150
R-3350-155
R-3350-160
R-3350-165
R-3350-170
R-3350-180
R-3350-185
R-3350-190
R-3350-94
gptkbp:firstFlight 1941
gptkbp:fuel_capacity wet sump
gptkbp:fuelType aviation gasoline
dual ignition
gptkbp:hasArea extensive testing during development
https://www.w3.org/2000/01/rdf-schema#label Wright R-3350 engine
gptkbp:is_used_in gptkb:Boeing_B-17_Flying_Fortress
gptkb:Lockheed_Constellation
gptkb:Boeing_B-29_Superfortress
gptkb:Douglas_DC-7
gptkbp:manufacturer gptkb:Wright_Aeronautical_Corporation
gptkbp:noise_level high noise levels
gptkbp:notable_feature twin-row design
gptkbp:performances high reliability
moderate maintenance requirements
up to 5,000 hours
high_altitude_performance
gptkbp:powerOutput 1,200 to 2,500 horsepower
gptkbp:productionYears 1941-1955
gptkbp:propulsion variable-pitch propeller
gptkbp:related_engine gptkb:Pratt_&_Whitney_R-2800
Wright_R-3000_series
gptkbp:setting two-row radial
gptkbp:successor gptkb:Wright_R-2600_engine
gptkbp:type radial engine
gptkbp:weight 1,800 pounds