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gptkbp:instance_of
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gptkb:turbofan_engine
|
|
gptkbp:application
|
gptkb:helicopter
civil helicopters
|
|
gptkbp:average_temperature
|
-40 to 50 ° C
|
|
gptkbp:certification
|
FAA certified
EASA certified
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compression_ratio
|
16:1
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
gptkb:FADEC
digital control system
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:development
|
gptkb:Leonardo_S.p._A.
gptkb:NATO
gptkb:Turbomeca
gptkb:Airbus
|
|
gptkbp:diameter
|
0.5 m
|
|
gptkbp:emissions_standard
|
gptkb:EURO_I
|
|
gptkbp:engine
|
gptkb:Turbomeca_Arriel
RTM series
|
|
gptkbp:engine_configuration
|
twin-spool
|
|
gptkbp:exhaust_system
|
gptkb:single
|
|
gptkbp:first_flight
|
gptkb:1990
|
|
gptkbp:fuel_economy
|
0.5 kg/s
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
dual fuel system
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Turbomeca RTM322
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:length
|
1.2 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Safran_Helicopter_Engines
|
|
gptkbp:market_segment
|
commercial
defense
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:number_of_stages
|
2
|
|
gptkbp:operational_range
|
500 km
|
|
gptkbp:operational_use
|
gptkb:search_and_rescue
anti-submarine warfare
reconnaissance missions
combat support
transport missions
|
|
gptkbp:power_output
|
1500 shp
|
|
gptkbp:propulsion
|
6:1
|
|
gptkbp:safety_features
|
redundant systems
|
|
gptkbp:service_ceiling
|
6000 m
|
|
gptkbp:turbine_type
|
gptkb:turbofan_engine
nickel alloy
|
|
gptkbp:type
|
gptkb:turbofan_engine
starter-generator
|
|
gptkbp:used_in
|
gptkb:Agusta_Westland_AW159_Wildcat
gptkb:Eurocopter_Tiger
gptkb:NHIndustries_NH90
|
|
gptkbp:weight
|
250 kg
|
|
gptkbp:bfsParent
|
gptkb:NH90_helicopter
|
|
gptkbp:bfsLayer
|
5
|