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gptkbp:instance_of
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gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:compression_ratio
|
6.5:1
|
|
gptkbp:configuration
|
V engine
|
|
gptkbp:control_system
|
mechanical throttle
|
|
gptkbp:cooling_system
|
liquid-cooled
water-cooled
|
|
gptkbp:displacement
|
24 liters
|
|
gptkbp:engine
|
500 hours
electric starter
influenced future aircraft engine designs
developed in the Soviet Union
used in various Soviet aircraft
|
|
gptkbp:engine_configuration
|
V-12
robust design
cradle mount
|
|
gptkbp:engine_power
|
1000 hours
high performance
high reliability
|
|
gptkbp:exhaust_system
|
gptkb:exhaust_system
|
|
gptkbp:first_flight
|
1947
|
|
gptkbp:fuel_capacity
|
0.9 m
1.5 m
0.8 m
|
|
gptkbp:fuel_economy
|
200 L/h
|
|
gptkbp:fuel_type
|
gptkb:carburetor
aviation gasoline
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Klimov VK-24 engine
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:maintenance
|
periodic maintenance required
|
|
gptkbp:manufacturer
|
Klimov
|
|
gptkbp:noise_level
|
low vibration
85 d B
|
|
gptkbp:number_of_engines
|
gptkb:12
|
|
gptkbp:power_output
|
2400 hp
|
|
gptkbp:produced_by
|
1947 to 1950
|
|
gptkbp:propeller
|
variable-pitch propeller
|
|
gptkbp:propulsion
|
4 hp/kg
|
|
gptkbp:replaced_by
|
gptkb:Klimov_VK-107_A
|
|
gptkbp:successor
|
gptkb:Klimov_VK-107
|
|
gptkbp:torque
|
pressure lubrication
flat torque curve
2000 Nm
|
|
gptkbp:type
|
V-12 piston engine
|
|
gptkbp:used_in
|
gptkb:Mikoyan-Gurevich_Mi_G-17
gptkb:Mikoyan-Gurevich_Mi_G-15
|
|
gptkbp:valve_configuration
|
overhead valve
|
|
gptkbp:weight
|
600 kg
|
|
gptkbp:bfsParent
|
gptkb:Klimov_design_bureau
|
|
gptkbp:bfsLayer
|
7
|