|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
helicopters
|
|
gptkbp:average_temperature
|
up to 900 ° C
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compressor_type
|
gptkb:3
axial
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design_date
|
gptkb:1965
|
|
gptkbp:diameter
|
0.9 m
|
|
gptkbp:emissions_standard
|
gptkb:Euro_I
|
|
gptkbp:engine
|
Brayton cycle
TV3 family
|
|
gptkbp:engine_configuration
|
inline
twin-spool
|
|
gptkbp:engine_power
|
3000 hours
|
|
gptkbp:engine_type
|
afterburning
TV3-117 VMA
TV3-117 VM
TV3-117 V
|
|
gptkbp:first_flight
|
gptkb:1970
|
|
gptkbp:fuel_economy
|
0.85 kg/k N·h
0.5 kg/k N·h
|
|
gptkbp:fuel_type
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Klimov TV3-117
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:length
|
1.8 m
|
|
gptkbp:maintenance
|
1000 hours
|
|
gptkbp:manufacturer
|
Klimov
|
|
gptkbp:max_speed
|
300 km/h
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:number_of_stages
|
8
|
|
gptkbp:operational_history
|
gptkb:Soviet_Union
|
|
gptkbp:power_output
|
1620 k W
|
|
gptkbp:production_status
|
in production
|
|
gptkbp:propulsion
|
14.67
2200 kgf
|
|
gptkbp:related_aircraft
|
gptkb:Mil_Mi-26
Kamov Ka-27
|
|
gptkbp:service_ceiling
|
6000 m
|
|
gptkbp:successor
|
gptkb:Klimov_VK-2500
|
|
gptkbp:turbine_type
|
2
axial
|
|
gptkbp:type
|
starter motor
twin-shaft engine
|
|
gptkbp:used_in
|
gptkb:Mil_Mi-24
gptkb:Mil_Mi-8
|
|
gptkbp:weight
|
150 kg
|
|
gptkbp:weight_to_thrust_ratio
|
0.068
|
|
gptkbp:bfsParent
|
gptkb:Ka-27_PL
gptkb:Ka-27_Helix
gptkb:Klimov_VK-2500
gptkb:Mil_Mi-171
|
|
gptkbp:bfsLayer
|
7
|