R-2800-94

GPTKB entity

Statements (52)
Predicate Object
gptkbp:instance_of gptkb:engine
gptkbp:bfsLayer 6
gptkbp:bfsParent gptkb:R-2800-77
gptkbp:aircraft_operated gptkb:Vought_F4_U_Corsair
gptkb:North_American_B-25_Mitchell
gptkb:Lockheed_P-38_Lightning
gptkbp:application gptkb:aircraft
gptkbp:compression_ratio 6.5:1
gptkbp:controls mechanical control
gptkbp:cooling_system air-cooled
direct air cooling
gptkbp:displacement 2800 cubic inches
gptkbp:engine gptkb:18
influential in aviation history
known for reliability
horizontally opposed
detailed specifications available
double row
radial layout
high performance ratings
periodic overhaul required
innovations in engine design
widely used in various aircraft
cradle mount
powerful engine for its time
Pratt & Whitney R-2800 family
characteristics well documented
mass production achieved
significant role in WWII aviation.
gptkbp:engine_type multiple variants produced
gptkbp:features two rows of nine cylinders
gptkbp:fuel_type aviation gasoline
carbureted
https://www.w3.org/2000/01/rdf-schema#label R-2800-94
gptkbp:ignition_system dual ignition
gptkbp:is_tested_for extensive testing conducted
gptkbp:maintenance routine maintenance required
gptkbp:manufacturer gptkb:Pratt_&_Whitney
gptkbp:original_run 1939
gptkbp:performance excellent
gptkbp:power_output 2000 to 2500 horsepower
gptkbp:production_years 1939 to 1960
gptkbp:propulsion variable pitch
gptkbp:reliability high
gptkbp:successor gptkb:R-4360_Wasp_Major
gptkbp:tuning tunable for performance
gptkbp:type gptkb:engine
gptkbp:used_in gptkb:aircraft
gptkb:Grumman_F8_F_Bearcat
gptkb:Douglas_DC-7
gptkbp:valve_configuration pushrod
gptkbp:weight approximately 1,600 pounds