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gptkbp:instance_of
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gptkb:engine
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|
gptkbp:bfsLayer
|
6
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gptkbp:bfsParent
|
gptkb:Sea_Hawk_Mk_122
gptkb:Sea_Hawk_Mk_125
gptkb:Sea_Hawk_Mk_146
gptkb:Turbomeca_Arriel_1_B
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|
gptkbp:application
|
helicopters
|
|
gptkbp:average_temperature
|
-40 to +50 ° C
|
|
gptkbp:certification
|
certified by EASA
|
|
gptkbp:controls
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:date
|
modern era
|
|
gptkbp:diameter
|
0.5 m
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissions_standard
|
low emissions
|
|
gptkbp:engine
|
gptkb:advanced_technology
high performance
commercial aviation
compact design
various options available
single engine
fuel efficient
quick startup time
smooth shutdown
proven reliability
Arriel family
used in various helicopter models
light helicopter engine
twin spool
|
|
gptkbp:engine_type
|
gptkb:engine
axial compressor
single stage turbine
2 B version
|
|
gptkbp:first_flight
|
gptkb:1980
|
|
gptkbp:fuel_capacity
|
120 kg
0.5 m
1.2 m
180 kg/h
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Turbomeca Arriel 2 B
|
|
gptkbp:launched
|
starter-generator
|
|
gptkbp:length
|
1.2 m
|
|
gptkbp:maintenance
|
500 hours
scheduled maintenance required
|
|
gptkbp:manufacturer
|
gptkb:Safran_Helicopter_Engines
|
|
gptkbp:noise_level
|
low noise level
|
|
gptkbp:notable_users
|
gptkb:Bell_407
Eurocopter A S350
Eurocopter E C130
|
|
gptkbp:power_consumption
|
600 shp
|
|
gptkbp:power_output
|
500 shp
|
|
gptkbp:powers
|
500 shp
4.2 k W/kg
|
|
gptkbp:propulsion
|
4.17 k W/kg
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_ceiling
|
3,000 m
|
|
gptkbp:setting
|
free turbine
|
|
gptkbp:weight
|
120 kg
|