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gptkbp:instance_of
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gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:aircraft
gptkb:military_aircraft
|
|
gptkbp:compression_ratio
|
6.5:1
|
|
gptkbp:configuration
|
supercharged
|
|
gptkbp:cooling_system
|
air-cooled
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|
gptkbp:displacement
|
3350 cubic inches
|
|
gptkbp:engine
|
single-stage
produced in large numbers
important in aviation history
influenced future engine designs
used in various aircraft types
|
|
gptkbp:engine_configuration
|
horizontally opposed
complex design features
|
|
gptkbp:engine_power
|
high power-to-weight ratio
proven in service
|
|
gptkbp:engine_type
|
multiple variants developed over time
|
|
gptkbp:first_flight
|
1941
|
|
gptkbp:fuel_capacity
|
approximately 6 ft 6 in
approximately 3 ft 6 in
approximately 4 ft 6 in
|
|
gptkbp:fuel_economy
|
variable based on load
|
|
gptkbp:fuel_type
|
aviation gasoline
carbureted
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Wright R-3350
|
|
gptkbp:ignition_system
|
dual ignition
|
|
gptkbp:is_tested_for
|
extensively tested before production
|
|
gptkbp:maintenance
|
periodic overhaul required
|
|
gptkbp:manufacturer
|
gptkb:Wright_Aeronautical_Corporation
|
|
gptkbp:noise_level
|
moderate vibration levels
notable for loud operation
|
|
gptkbp:number_of_engines
|
gptkb:18
|
|
gptkbp:operational_range
|
1,800 to 3,000 rpm
|
|
gptkbp:power_output
|
up to 2,500 hp
|
|
gptkbp:production_years
|
1941-1955
|
|
gptkbp:propulsion
|
significant thrust generation
|
|
gptkbp:successor
|
gptkb:Wright_R-4360
|
|
gptkbp:torque
|
high torque output
wet sump
|
|
gptkbp:type
|
gptkb:radial_engine
|
|
gptkbp:used_in
|
gptkb:Lockheed_Constellation
gptkb:Boeing_B-17_Superfortress
gptkb:Douglas_DC-7
gptkb:Boeing_Stratocruiser
|
|
gptkbp:valve_configuration
|
pushrod
|
|
gptkbp:variant
|
gptkb:R-3350-26
gptkb:R-3350-32
R-3350-57
R-3350-23
|
|
gptkbp:weight
|
approximately 1,800 lbs
|
|
gptkbp:bfsParent
|
gptkb:Bockscar
gptkb:B-29_Superfortress
gptkb:Douglas_A-1_Skyraider
gptkb:Enola_Gay
|
|
gptkbp:bfsLayer
|
4
|