Statements (58)
Predicate | Object |
---|---|
gptkbp:instance_of |
gptkb:engine
|
gptkbp:bfsLayer |
6
|
gptkbp:bfsParent |
gptkb:Continental_AV-1790
|
gptkbp:application |
gptkb:aircraft
|
gptkbp:bore |
5.5 inches
|
gptkbp:compression_ratio |
7.0:1
|
gptkbp:controls |
mechanical
|
gptkbp:cooling_system |
gptkb:fandom
liquid-cooled water-cooled water-cooled system |
gptkbp:displacement |
1,790 cubic inches
|
gptkbp:emissions_standard |
pre-1970 standards
|
gptkbp:engine |
cast iron
naturally aspirated high performance for its time developed during WWII dual ignition system detailed specifications available aircraft engine design used in various military applications 2,600 RPM V12 layout 750 hp at 2,600 RPM known for reliability in combat tank propulsion cradle-mounted 750 hp at max RPM influenced future tank engines used in M48 and M60 tanks |
gptkbp:engine_type |
reciprocating engine
AV-1790-1, AV-1790-2 |
gptkbp:first_introduced |
1945
|
gptkbp:fuel_capacity |
variable based on load
|
gptkbp:fuel_type |
gptkb:Company
carbureted gasoline fuel |
https://www.w3.org/2000/01/rdf-schema#label |
Continental AV-1790-19
|
gptkbp:ignition_system |
distributor ignition
|
gptkbp:is_designed_to |
armored vehicles
|
gptkbp:maintenance |
requires regular maintenance
|
gptkbp:manufacturer |
gptkb:Continental_Motors
|
gptkbp:notable_features |
high power-to-weight ratio
|
gptkbp:power_output |
750 horsepower
|
gptkbp:produced_by |
gptkb:1980s
|
gptkbp:production_years |
1940s to 1980s
|
gptkbp:related_to |
gptkb:Continental_AV-1790
|
gptkbp:replaced_by |
MTUMB 871
|
gptkbp:setting |
V engine
|
gptkbp:stroke |
6.0 inches
|
gptkbp:successor |
gptkb:Continental_AV-1790-2
|
gptkbp:torque |
1,500 lb-ft
1,500 lb-ft at 1,600 RPM 1,500 lb-ft at max RPM |
gptkbp:type |
gptkb:engine
|
gptkbp:used_in |
gptkb:M60_tank
|
gptkbp:valve_configuration |
overhead valve
|
gptkbp:weight |
1,800 lbs
|