Avia M-137 engine

GPTKB entity

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