|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:aircraft
gptkb:military_aircraft
|
|
gptkbp:compression_ratio
|
6.5:1
|
|
gptkbp:configuration
|
two-row radial engine
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:displacement
|
3,350 cubic inches
|
|
gptkbp:engine
|
two-speed supercharger
single-stage turbocharger
R-10000 series
R-3000 series
R-4000 series
R-5000 series
R-6000 series
R-7000 series
R-8000 series
R-9000 series
|
|
gptkbp:engine_configuration
|
14-cylinder
horizontally opposed
|
|
gptkbp:engine_type
|
piston engine
|
|
gptkbp:first_flight
|
1941
|
|
gptkbp:fuel_capacity
|
approximately 3.5 feet
approximately 6 feet
wet sump
|
|
gptkbp:fuel_type
|
aviation gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Wright R-3350 series
|
|
gptkbp:ignition_system
|
dual ignition
|
|
gptkbp:manufacturer
|
gptkb:Wright_Aeronautical_Corporation
|
|
gptkbp:notable_users
|
gptkb:Royal_Air_Force
gptkb:Trans_World_Airlines
gptkb:United_Airlines
gptkb:United_States_Navy
gptkb:Pan_American_World_Airways
|
|
gptkbp:power_output
|
1,200 to 2,500 horsepower
|
|
gptkbp:production_years
|
1941 to 1955
|
|
gptkbp:successor
|
gptkb:Wright_R-4360
|
|
gptkbp:type
|
gptkb:radial_engine
|
|
gptkbp:used_in
|
gptkb:Lockheed_Constellation
gptkb:Boeing_B-17_Superfortress
gptkb:Douglas_DC-7
|
|
gptkbp:valve_configuration
|
double overhead camshaft
|
|
gptkbp:variant
|
gptkb:R-3350-32
R-3350-57
R-3350-23
R-3350-26 W
|
|
gptkbp:weight
|
approximately 1,800 pounds
|
|
gptkbp:bfsParent
|
gptkb:Wright_R-1820_Cyclone
|
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gptkbp:bfsLayer
|
5
|