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gptkbp:instance_of
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gptkb:turbofan_engine
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gptkbp:aircraft_type
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gptkb:helicopter
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gptkbp:application
|
civil and military helicopters
|
|
gptkbp:average_temperature
|
high operating temperature
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gptkbp:certification
|
EASA certified
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gptkbp:combustor_type
|
annular combustion chamber
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gptkbp:components
|
modular component design
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gptkbp:compression_ratio
|
16:1
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gptkbp:control_system
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gptkb:full_authority_digital_engine_control_(FADEC)
digital engine control system
|
|
gptkbp:cooling_system
|
air-cooled
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|
gptkbp:customer_base
|
global customer base
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gptkbp:design_purpose
|
medium to heavy helicopters
|
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gptkbp:development
|
developed from Makila 2 engine
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gptkbp:diameter
|
600 mm
|
|
gptkbp:emissions_standard
|
low emissions
|
|
gptkbp:engine_configuration
|
twin-spool configuration
|
|
gptkbp:environmental_impact
|
reduced environmental impact
|
|
gptkbp:first_flight
|
gptkb:2005
|
|
gptkbp:fuel_economy
|
high fuel efficiency
low fuel consumption
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
gptkbp:gearbox
|
integrated gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Makila 1 U engine
|
|
gptkbp:innovation
|
continuous innovation in design
|
|
gptkbp:launch_window
|
electrical starter
|
|
gptkbp:legal_principle
|
gas turbine principle
|
|
gptkbp:length
|
1,200 mm
|
|
gptkbp:maintenance
|
3,500 hours
|
|
gptkbp:manufacturer
|
gptkb:Safran_Helicopter_Engines
|
|
gptkbp:market_position
|
high spare parts availability
|
|
gptkbp:market_segment
|
commercial aviation
|
|
gptkbp:noise_level
|
low noise level
|
|
gptkbp:operational_range
|
long operational range
|
|
gptkbp:operational_use
|
used in offshore operations
|
|
gptkbp:performance
|
meets performance metrics
|
|
gptkbp:power_output
|
1,800 shp at takeoff
|
|
gptkbp:propulsion
|
high power-to-weight ratio
1,800 shp
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_ceiling
|
high service ceiling
|
|
gptkbp:services_provided
|
comprehensive support services
|
|
gptkbp:training_programs
|
training programs for operators
|
|
gptkbp:turbine_efficiency
|
high turbine efficiency
|
|
gptkbp:turbine_type
|
advanced composite materials
two-stage gas generator
|
|
gptkbp:type
|
turbo-shaft
|
|
gptkbp:used_in
|
gptkb:Eurocopter_EC225_Super_Puma
|
|
gptkbp:weight
|
about 300 kg
|
|
gptkbp:bfsParent
|
gptkb:Safran_Helicopter_Engines
|
|
gptkbp:bfsLayer
|
5
|