|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:aircraft_operated
|
gptkb:Lockheed_Constellation
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:compression_ratio
|
6:1
|
|
gptkbp:configuration
|
14-cylinder
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:country_of_origin
|
gptkb:United_States
|
|
gptkbp:displacement
|
1,200 cubic inches
|
|
gptkbp:engine
|
gptkb:military_aircraft
gptkb:Wright_Aeronautical_Corporation
gptkb:Wright_R-series
R-series
|
|
gptkbp:engine_configuration
|
horizontally opposed
radial layout
radial configuration
|
|
gptkbp:engine_displacement
|
1,200 in³
|
|
gptkbp:engine_power
|
1,200 hp
2,400 RPM
|
|
gptkbp:engine_rpm_rating
|
2,400 RPM
|
|
gptkbp:engine_torque_rating
|
1,200 lb-ft
|
|
gptkbp:engine_type
|
R-2
reciprocating engine
|
|
gptkbp:first_flight
|
1936
|
|
gptkbp:first_introduced
|
gptkb:Boeing_B-17_Flying_Fortress
|
|
gptkbp:fuel_capacity
|
3.5 feet
1,200 lbs
3.5 ft
4.5 ft
4.5 feet
|
|
gptkbp:fuel_economy
|
0.5 pounds per horsepower per hour
|
|
gptkbp:fuel_type
|
aviation gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Wright R-2
|
|
gptkbp:ignition_system
|
dual ignition
|
|
gptkbp:manufacturer
|
gptkb:Wright_Aeronautical_Corporation
|
|
gptkbp:number_of_engines
|
gptkb:14
|
|
gptkbp:power_output
|
1,200 horsepower
|
|
gptkbp:production_years
|
1936-1945
|
|
gptkbp:propeller
|
variable-pitch propeller
|
|
gptkbp:replaced_by
|
gptkb:Wright_R-2600
|
|
gptkbp:successor
|
gptkb:Wright_R-3350
|
|
gptkbp:torque
|
1,200 lb-ft
|
|
gptkbp:type
|
gptkb:radial_engine
|
|
gptkbp:used_in
|
gptkb:Boeing_B-17_Flying_Fortress
|
|
gptkbp:weight
|
1,200 pounds
|
|
gptkbp:bfsParent
|
gptkb:Wright_R-1
|
|
gptkbp:bfsLayer
|
8
|