Wright R-975-N1

GPTKB entity

Statements (51)
Predicate Object
gptkbp:instance_of gptkb:jet_engine
gptkbp:application gptkb:military_aircraft
civil aircraft
gptkbp:bore 5.5 inches
gptkbp:compression_ratio 6.5:1
gptkbp:configuration air-cooled
gptkbp:cooling_system air-cooled
air cooling
air-cooled method
gptkbp:displacement 975 cubic inches
gptkbp:engine gptkb:Wright_R-900_series
gptkb:Wright_R-975_family
significant in aviation history
legacy in military aviation
developed during the 1930s
gptkbp:engine_configuration 9-cylinder
radial layout
radial design
detailed specifications available.
gptkbp:engine_operational_altitude operational at various altitudes
gptkbp:engine_power high reliability
high power-to-weight ratio
long lifespan
gptkbp:engine_torque_characteristics good torque characteristics
gptkbp:engine_type reciprocating engine
several variants produced
gptkbp:fuel_economy moderate fuel consumption
gptkbp:fuel_type aviation gasoline
https://www.w3.org/2000/01/rdf-schema#label Wright R-975-N1
gptkbp:ignition_system magneto ignition
gptkbp:maintenance moderate maintenance requirements
gptkbp:manufacturer gptkb:Wright_Aeronautical_Corporation
gptkbp:noise_level moderate vibration
notable noise level
gptkbp:number_of_engines gptkb:9
gptkbp:original_run 1930s
gptkbp:power_output 450 horsepower
gptkbp:production_years 1930s to 1940s
gptkbp:propeller variable-pitch propeller
gptkbp:propulsion significant thrust generation
gptkbp:stroke 6.0 inches
gptkbp:successor gptkb:Wright_R-1820
gptkbp:torque high torque output
gptkbp:type gptkb:radial_engine
gptkbp:used_in gptkb:Boeing_B-17_Flying_Fortress
gptkb:C-46_Commando
gptkb:P-47_Thunderbolt
gptkbp:valve_configuration pushrod
gptkbp:weight approximately 600 pounds
gptkbp:bfsParent gptkb:Wright_R-975
gptkbp:bfsLayer 7