|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
helicopters
|
|
gptkbp:average_temperature
|
400 ° C
|
|
gptkbp:compression_ratio
|
16:1
|
|
gptkbp:compressor_type
|
5 stages
axial compressor
|
|
gptkbp:control_system
|
gptkb:FADEC
digital control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design_purpose
|
helicopter propulsion
|
|
gptkbp:diameter
|
0.4 m
4000 RPM
|
|
gptkbp:emissions_standard
|
ICAO Chapter 4
|
|
gptkbp:engine
|
Brayton cycle
|
|
gptkbp:engine_configuration
|
flexible mount
single spool
single shaft
|
|
gptkbp:engine_power
|
3000 hours
4000 RPM
600 k W
|
|
gptkbp:engine_shutdown_time
|
10 seconds
|
|
gptkbp:engine_start_time
|
30 seconds
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
|
|
gptkbp:exhaust_temperature
|
600 ° C
|
|
gptkbp:first_flight
|
gptkb:1970
|
|
gptkbp:fuel_capacity
|
150 kg
200 liters
1.2 m x 0.4 m
|
|
gptkbp:fuel_economy
|
high
0.5 kg/k W·h
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
gptkb:gasoline
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Turbomeca TM 319
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:launch_window
|
electric starter
|
|
gptkbp:length
|
1.2 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Turbomeca
|
|
gptkbp:noise_level
|
low
85 d B
|
|
gptkbp:operational_range
|
1000 km
|
|
gptkbp:power_output
|
600 k W
|
|
gptkbp:propulsion
|
20:1
3190 lbf
|
|
gptkbp:service_ceiling
|
6000 m
|
|
gptkbp:torque
|
800 Nm
|
|
gptkbp:turbine_type
|
free turbine
2 stages
nickel alloy
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Eurocopter_AS350
|
|
gptkbp:weight
|
150 kg
200 kg
|
|
gptkbp:bfsParent
|
gptkb:Rolls-Royce_Turbomeca_Adour
gptkb:Brunei_Air_Force
gptkb:Cheetah_helicopter
|
|
gptkbp:bfsLayer
|
6
|