Statements (53)
Predicate | Object |
---|---|
gptkbp:instance_of |
gptkb:engine
|
gptkbp:bfsLayer |
8
|
gptkbp:bfsParent |
gptkb:Zlin_Z-526_A
|
gptkbp:application |
gptkb:aircraft
|
gptkbp:compression_ratio |
6.5:1
|
gptkbp:controls |
mechanical control
|
gptkbp:cooling_system |
gptkb:fandom
liquid-cooled water-cooled |
gptkbp:displacement |
137 liters
|
gptkbp:engine |
gptkb:12
high performance various aircraft types used in World War II electric starter V configuration reliable engine dual ignition system influenced future designs detailed specifications available innovative design features air-cooled design limited production run developed in the 1930s V12 configuration performance metrics available. used in combat aircraft cradle mount 600 hp at 2800 RPM |
gptkbp:engine_type |
multiple variants produced
|
gptkbp:first_flight |
1937
|
gptkbp:fuel_capacity |
high fuel consumption
heavy engine |
gptkbp:fuel_type |
aviation gasoline
|
https://www.w3.org/2000/01/rdf-schema#label |
Avia M-137 engine
|
gptkbp:ignition_system |
magneto ignition
|
gptkbp:is_tested_for |
extensively tested
|
gptkbp:maintenance |
periodic maintenance required
|
gptkbp:manufacturer |
Avia
|
gptkbp:max_speed |
2800 RPM
|
gptkbp:origin |
gptkb:Monarch
|
gptkbp:powers |
600 horsepower
|
gptkbp:production_years |
1937-1945
|
gptkbp:propulsion |
variable-pitch propeller
1.5 hp/kg |
gptkbp:setting |
gptkb:V12
|
gptkbp:successor |
Avia M-139 engine
|
gptkbp:torque |
500 Nm
high torque output |
gptkbp:type |
piston engine
|
gptkbp:used_in |
gptkb:Avia_B-534
|
gptkbp:valve_configuration |
overhead valve
|
gptkbp:weight |
400 kg
|