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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:military_aircraft
civil aircraft
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gptkbp:compression_ratio
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6.5:1
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gptkbp:configuration
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14-cylinder
Two-row radial
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gptkbp:cooling_system
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air-cooled
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gptkbp:diameter
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48 inches
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gptkbp:displacement
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2,600 cubic inches
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gptkbp:engine
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gptkb:World_War_II_aircraft
gptkb:Wright_R-1820
gptkb:R-2600_series
gptkb:Wright_Cyclone
dual ignition system
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gptkbp:engine_configuration
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gptkb:Wright_Aeronautical
horizontally opposed
radial layout
two-row radial
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gptkbp:engine_displacement
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2,600 in³
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gptkbp:engine_power
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1,600 hp
high reliability
high power-to-weight ratio
2,700 RPM
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gptkbp:engine_type
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reciprocating engine
R-2600-11
R-2600-13
R-2600-3
R-2600-7
R-2600-15
R-2600-19
R-2600-23
R-2600-27
R-2600-29
R-2600-31
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gptkbp:first_flight
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1939
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gptkbp:fuel_capacity
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1,600 lb
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gptkbp:fuel_type
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aviation gasoline
carbureted
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|
https://www.w3.org/2000/01/rdf-schema#label
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Wright R-2600 Cyclone
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gptkbp:ignition_system
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dual ignition
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gptkbp:length
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54 inches
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gptkbp:manufacturer
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gptkb:Wright_Aeronautical_Corporation
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gptkbp:notable_feature
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two-row design
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gptkbp:number_of_engines
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gptkb:14
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gptkbp:original_run
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1939
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gptkbp:power_output
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1,600 horsepower
1,700 horsepower
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gptkbp:production_years
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1939-1945
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gptkbp:propeller
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variable-pitch propeller
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gptkbp:successor
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gptkb:Wright_R-3350
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gptkbp:torque
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high torque
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gptkbp:type
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gptkb:radial_engine
Radial engine
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gptkbp:used_in
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gptkb:Boeing_B-17_Flying_Fortress
gptkb:Lockheed_Hudson
gptkb:Douglas_A-20_Havoc
gptkb:B-24_Liberator
gptkb:Boeing_B-17_G
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gptkbp:valve_configuration
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pushrod
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gptkbp:weight
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1,600 pounds
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gptkbp:bfsParent
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gptkb:Curtiss_SB2_C_Helldiver
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gptkbp:bfsLayer
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4
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