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gptkbp:instance_of
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gptkb:jet_engine
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|
gptkbp:application
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gptkb:aircraft
gptkb:military_aircraft
|
|
gptkbp:bore
|
5.5 inches
|
|
gptkbp:compression_ratio
|
6.5:1
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|
gptkbp:configuration
|
18-cylinder
|
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gptkbp:cooling_system
|
air-cooled
air-cooled engine
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|
gptkbp:displacement
|
4360 cubic inches
|
|
gptkbp:engine
|
gptkb:Convair_340
gptkb:Wright_Aeronautical_Corporation
gptkb:Lockheed_Constellation
gptkb:Boeing_B-17
gptkb:Douglas_DC-7
high power output
1940-1955
dual ignition system
supercharged engine
air-cooled design
pushrod actuated valves
carbureted fuel system
horizontally opposed layout
|
|
gptkbp:engine_configuration
|
horizontally opposed
radial configuration
18-cylinder engine
|
|
gptkbp:engine_displacement
|
4,360 in³
|
|
gptkbp:engine_power
|
3,000 hp
|
|
gptkbp:engine_type
|
gptkb:radial_engine
reciprocating engine
|
|
gptkbp:first_flight
|
gptkb:1940
|
|
gptkbp:fuel_capacity
|
1,800 lbs
|
|
gptkbp:fuel_type
|
aviation gasoline
carbureted
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Wright R-4360
|
|
gptkbp:ignition_system
|
dual ignition
|
|
gptkbp:manufacturer
|
gptkb:Wright_Aeronautical_Corporation
|
|
gptkbp:notable_feature
|
supercharged
|
|
gptkbp:number_of_engines
|
gptkb:18
|
|
gptkbp:power_output
|
3000 horsepower
|
|
gptkbp:production_years
|
1940-1955
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|
gptkbp:stroke
|
6.5 inches
|
|
gptkbp:successor
|
gptkb:Wright_R-3350
|
|
gptkbp:type
|
gptkb:radial_engine
|
|
gptkbp:used_in
|
gptkb:Convair_340
gptkb:Boeing_B-17_Flying_Fortress
gptkb:Lockheed_Constellation
gptkb:Douglas_DC-7
|
|
gptkbp:valve_configuration
|
pushrod actuated
|
|
gptkbp:weight
|
approximately 1,800 pounds
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gptkbp:bfsParent
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gptkb:Wright_R-3350
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gptkbp:bfsLayer
|
5
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