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
|