Statements (52)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:jet_engine
|
| gptkbp:application |
gptkb:military_aircraft
|
| gptkbp:compression_ratio |
6.5:1
|
| gptkbp:configuration |
liquid-cooled
|
| gptkbp:cooling_system |
liquid cooling
water-cooled |
| gptkbp:displacement |
1,570 cubic inches
|
| gptkbp:engine |
limited production
four-stroke influential in aviation history various aircraft innovative design features developed in the 1920s faced engineering challenges used in various military aircraft historically significant engine well-regarded engine Conqueror series contributed to engine advancements. |
| gptkbp:engine_configuration |
V engine
naturally aspirated detailed specifications available aircraft engine design distinctive characteristics |
| gptkbp:engine_power |
high performance
reliable engine performance metrics documented |
| gptkbp:engine_production_numbers |
limited production numbers
|
| gptkbp:engine_type |
reciprocating engine
several variants |
| gptkbp:fuel_capacity |
dry sump
|
| gptkbp:fuel_type |
aviation gasoline
|
| https://www.w3.org/2000/01/rdf-schema#label |
Curtiss V-1570 Conqueror
|
| gptkbp:ignition_system |
gptkb:Champion
dual ignition |
| gptkbp:intended_use |
racing and military aviation
|
| gptkbp:is_tested_for |
extensively tested
|
| gptkbp:manufacturer |
gptkb:Curtiss_Aeroplane_and_Motor_Company
|
| gptkbp:notable_feature |
high power-to-weight ratio
|
| gptkbp:number_of_engines |
gptkb:12
|
| gptkbp:original_run |
1928
|
| gptkbp:power_output |
600 horsepower
|
| gptkbp:production_years |
1928-1935
|
| gptkbp:successor |
gptkb:Curtiss_V-1570-1_Conqueror
|
| gptkbp:type |
V-12 engine
|
| gptkbp:used_in |
gptkb:Curtiss_P-6_Hawk
gptkb:Curtiss_R3_C-2_Racer |
| gptkbp:valve_configuration |
overhead valves
|
| gptkbp:weight |
approximately 800 pounds
|
| gptkbp:bfsParent |
gptkb:Curtiss_P-36_Hawk
gptkb:P-36_Hawk |
| gptkbp:bfsLayer |
6
|