Pratt & Whitney R-2000 family

GPTKB entity

Statements (65)
Predicate Object
gptkbp:instance_of gptkb:jet_engine
gptkbp:application gptkb:Douglas_DC-3
gptkb:Convair_240
gptkb:Boeing_307_Stratoliner
gptkb:Lockheed_Lodestar
Martin 404
gptkbp:certification FAA certified
gptkbp:compression_ratio 6.5:1
gptkbp:control_system manual throttle control
gptkbp:cooling_system air-cooled
gptkbp:displacement 1,200 cubic inches
gptkbp:engine gptkb:R-2000_family
gptkbp:engine_configuration horizontally opposed
single-row radial
gptkbp:engine_power high reliability
approximately 1,500 hours
moderate fuel efficiency
gptkbp:engine_type R-2000-16
R-2000-19
R-2000-1
R-2000-13
R-2000-15
R-2000-17
R-2000-18
R-2000-20
R-2000-10
R-2000-12
R-2000-2
R-2000-3
R-2000-4
R-2000-5
R-2000-6
R-2000-8
R-2000-9
gptkbp:first_flight gptkb:1940
gptkbp:fuel_capacity wet sump
gptkbp:fuel_type aviation gasoline
gravity feed
https://www.w3.org/2000/01/rdf-schema#label Pratt & Whitney R-2000 family
gptkbp:ignition_system dual ignition
gptkbp:is_tested_for extensive ground testing conducted
gptkbp:maintenance periodic overhaul required
gptkbp:manufacturer gptkb:Pratt_&_Whitney
gptkbp:noise_level notable noise levels
gptkbp:notable_users gptkb:Trans_World_Airlines
gptkb:United_States_Air_Force
gptkb:Eastern_Air_Lines
gptkb:Pan_American_World_Airways
gptkb:Western_Airlines
gptkbp:number_of_engines 9-cylinder
gptkbp:power_output 1,200 to 1,400 horsepower
gptkbp:production_years 1940 to 1950s
gptkbp:propeller variable-pitch propeller
gptkbp:replaced_by turboprop engines
gptkbp:successor gptkb:Pratt_&_Whitney_R-2800
gptkbp:type gptkb:radial_engine
gptkbp:used_in gptkb:military_aircraft
civilian aircraft
gptkbp:valve_configuration overhead valves
gptkbp:variant R-2000-11
R-2000-14
R-2000-7
gptkbp:weight approximately 1,200 pounds
gptkbp:bfsParent gptkb:Pratt_&_Whitney_R-2000
gptkbp:bfsLayer 5