Wright R-3350-26 B

GPTKB entity

Statements (48)
Predicate Object
gptkbp:instance_of gptkb:jet_engine
gptkbp:application gptkb:military_aircraft
commercial aviation
gptkbp:availability available in surplus markets
gptkbp:compression_ratio 7.0:1
gptkbp:control_system mechanical control system
gptkbp:cooling_system air-cooled
uses oil for cooling
gptkbp:cultural_impact featured in aviation museums
gptkbp:design_features designed for high altitude performance
gptkbp:displacement 3350 cubic inches
gptkbp:engine yes
produced in large numbers
requires external power for start
gptkbp:engine_configuration horizontally opposed
detailed specifications available
radial layout
double-row radial engine
gptkbp:engine_power maximum RPM 2700
notable for power-to-weight ratio
gptkbp:engine_testing_duration long testing duration
gptkbp:engine_type multiple variants produced
gptkbp:first_flight 1941
gptkbp:fuel_economy high fuel consumption
gptkbp:fuel_type aviation gasoline
gptkbp:historical_significance important in aviation history
https://www.w3.org/2000/01/rdf-schema#label Wright R-3350-26 B
gptkbp:is_tested_for extensively tested before production
tested at Wright Field
gptkbp:legacy influenced future aircraft engine designs
gptkbp:maintenance requires regular maintenance
gptkbp:manufacturer gptkb:Wright_Aeronautical_Corporation
gptkbp:notable_feature gptkb:turbofan_engine
gptkbp:number_of_engines gptkb:18
double-row
gptkbp:operational_history used in World War II
used in the Korean War
gptkbp:power_output 2000 horsepower
gptkbp:propeller variable-pitch propeller
gptkbp:reliability high reliability
gptkbp:retirement retired from service in the 1960s
gptkbp:successor Wright R-3350-26 C
gptkbp:torque high torque output
gptkbp:type gptkb:radial_engine
gptkbp:used_in gptkb:Lockheed_Constellation
gptkb:Boeing_B-17_Superfortress
gptkb:Douglas_DC-7
gptkbp:weight approximately 1,800 pounds