Turbomeca Arrius 2 F

GPTKB entity

Statements (80)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkbp:application helicopters
helicopter propulsion
gptkbp:average_temperature 900 ° C
1,000 ° C
gptkbp:certification gptkb:EASA
EASA certified
gptkbp:compression_ratio 16:1
gptkbp:compressor_type axial
axial compressor
gptkbp:control_system gptkb:FADEC
digital electronic control
gptkbp:cooling_system air-cooled
gptkbp:design_purpose gptkb:civil_aviation
gptkbp:diameter 0.5 m
0.4 m
gptkbp:elevation 3000 m
up to 20,000 ft
gptkbp:emissions_standard low
low emissions
ICAO Chapter 4
gptkbp:engine Turbomeca Arrius 2 B
electric starter motor
gptkbp:engine_configuration free turbine
single-shaft
gptkbp:engine_operational_altitude 20,000 ft
gptkbp:engine_power high reliability
3000 hours
500 shp
gptkbp:engine_service_entry_year gptkb:1980
gptkbp:engine_type turbo-shaft
Arrius 2 B
gptkbp:exhaust_system gptkb:straight
straight exhaust
gptkbp:first_flight gptkb:1980
gptkbp:fuel_capacity 120 kg
0.5 m
1.2 m
1.1 m
0.4 m
gptkbp:fuel_economy 0.5 kg/shp/h
0.5 kg/k W·h
gptkbp:fuel_type gptkb:electronic
gptkb:Jet_A-1
gptkbp:gearbox reduction gearbox
https://www.w3.org/2000/01/rdf-schema#label Turbomeca Arrius 2 F
gptkbp:ignition_system spark ignition
gptkbp:launch_window electric starter
starter-generator
gptkbp:length 1.2 m
1.1 m
gptkbp:maintenance 500 hours
gptkbp:manufacturer gptkb:Turbomeca
gptkbp:max_speed 42,000
gptkbp:noise_level low
low noise
85 d B
gptkbp:notable_users gptkb:Airbus
gptkbp:number_of_stages 2
gptkbp:power_output 500 shp
370 k W
gptkbp:propulsion 500 shp
4.17 shp/kg
gptkbp:reliability high
gptkbp:service_entry gptkb:1980
gptkbp:turbine_type 2
single-spool
free turbine
nickel alloy
gptkbp:type gptkb:turbofan_engine
turbo-shaft
gptkbp:used_in gptkb:Eurocopter_AS350
gptkbp:variant Arrius 2 B
gptkbp:water_requirement 100 kg/h
gptkbp:weight 120 kg
150 kg
gptkbp:bfsParent gptkb:EC120_B
gptkb:EC120_Colibri
gptkb:Eurocopter_EC120
gptkbp:bfsLayer 6