|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
civil helicopters
|
|
gptkbp:average_temperature
|
1,200 ° C
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compression_ratio
|
16:1
|
|
gptkbp:configuration
|
free turbine
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
gptkb:FADEC
digital electronic control
|
|
gptkbp:cooling_system
|
gptkb:oil
liquid cooling
air-cooled
|
|
gptkbp:design_purpose
|
medium lift helicopters
|
|
gptkbp:diameter
|
600 mm
|
|
gptkbp:elevation
|
up to 15,000 ft
|
|
gptkbp:emissions_standard
|
EURO 1
|
|
gptkbp:engine
|
air start
|
|
gptkbp:engine_configuration
|
twin-engine configuration
flexible mount
|
|
gptkbp:engine_power
|
5,000 hours
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
|
|
gptkbp:first_flight
|
gptkb:2005
|
|
gptkbp:fuel_economy
|
high
200 kg/h
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Makila 1 N engine
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:launch_platform
|
electrical starter
|
|
gptkbp:length
|
1,200 mm
|
|
gptkbp:maintenance
|
1,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Safran_Helicopter_Engines
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:operational_range
|
1,000 km
|
|
gptkbp:power_output
|
1,800 shp
|
|
gptkbp:propulsion
|
5:1
6 hp/kg
|
|
gptkbp:reduction_gear
|
planetary gear system
|
|
gptkbp:service_ceiling
|
up to 20,000 ft
|
|
gptkbp:torque
|
1,800 Nm
|
|
gptkbp:turbine_type
|
single-spool
|
|
gptkbp:type
|
turboshaft
|
|
gptkbp:used_in
|
gptkb:Eurocopter_EC225_Super_Puma
|
|
gptkbp:weight
|
about 300 kg
|
|
gptkbp:bfsParent
|
gptkb:Safran_Helicopter_Engines
|
|
gptkbp:bfsLayer
|
5
|