Statements (51)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
gptkb:military_aircraft
|
| gptkbp:bore |
4.0 inches
|
| gptkbp:compression_ratio |
6.5:1
|
| gptkbp:configuration |
liquid-cooled
|
| gptkbp:cooling_system |
gptkb:Cooler
water-cooled |
| gptkbp:displacement |
1,570 cubic inches
|
| gptkbp:engine |
part of aviation history
influenced future designs used in various aircraft models faced engineering challenges unique design features produced in limited numbers 600 hp at 2,600 rpm introduced several innovations contributed to advancements in technology Curtiss Conqueror operational use in military |
| gptkbp:engine_configuration |
V engine
inline engine design detailed specifications available V-12 configuration distinctive characteristics |
| gptkbp:engine_power |
high performance
limited lifespan reliable engine performance metrics documented |
| gptkbp:engine_type |
reciprocating engine
multiple variants available |
| gptkbp:fuel_capacity |
heavy engine
|
| gptkbp:fuel_type |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Curtiss V-1570-2 Conqueror
|
| gptkbp:intended_use |
gptkb:fighter_aircraft
|
| gptkbp:is_tested_for |
extensively tested
|
| gptkbp:maintenance |
requires regular maintenance
|
| gptkbp:manufacturer |
gptkb:Curtiss_Aeroplane_and_Motor_Company
|
| gptkbp:notable_features |
high power-to-weight ratio
|
| gptkbp:original_run |
1930s
|
| gptkbp:power_output |
600 horsepower
|
| gptkbp:production_years |
1930s to 1940s
|
| gptkbp:related_aircraft |
gptkb:Curtiss_P-40_Warhawk
|
| gptkbp:stroke |
4.0 inches
|
| gptkbp:successor |
Curtiss V-1570-3 Conqueror
|
| gptkbp:torque |
high torque
|
| gptkbp:type |
V-12 engine
|
| gptkbp:used_in |
gptkb:Curtiss_P-6_Hawk
|
| gptkbp:valve_configuration |
overhead valves
|
| gptkbp:weight |
approximately 800 pounds
|
| gptkbp:bfsParent |
gptkb:Curtiss_V-1570-1_Conqueror
|
| gptkbp:bfsLayer |
8
|