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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:Turbomeca_Arriel_1_B
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|
gptkbp:accessories
|
gptkb:Company
gptkb:military_base
gptkb:starship
gptkb:engine
gptkb:railway_station
temperature sensors
control unit
pressure sensors
speed sensors
vibration sensors
oil cooler
fuel filter
fuel flow meter
starter generator
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|
gptkbp:application
|
gptkb:Bell_407
gptkb:Agusta_A109
A S350 Écureuil
Eurocopter A S350
Eurocopter E C120 Colibri
Eurocopter E C120
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|
gptkbp:average_temperature
|
-40 to 50 ° C
up to 700 ° C
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|
gptkbp:certification
|
gptkb:EASA
gptkb:FAA
EASA certified
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|
gptkbp:clutch_size
|
15:1
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|
gptkbp:compression_ratio
|
16:1
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|
gptkbp:controls
|
gptkb:football_match
digital electronic control
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|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
5000 hours
|
|
gptkbp:diameter
|
0.4 m
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:elevation
|
up to 3000 m
|
|
gptkbp:emissions_standard
|
single exhaust
ICAO Chapter 4
|
|
gptkbp:engine
|
gptkb:Turbomeca_Arriel_1_M
gptkb:Turbomeca_Arriel_1_H
gptkb:Turbomeca_Arriel_1_S
gptkb:Turbomeca_Arriel_1_B
high reliability
3000 hours
free turbine
flexible mount
single spool
cool down required
hot start capable
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|
gptkbp:engine_type
|
gptkb:Arriel_1_B
gptkb:Arriel_1_M
gptkb:Arriel_2_B
gptkb:Arriel_2_M
gptkb:Arriel_2_S
gptkb:3
2
axial compressor
single-stage turbine
turbo-shaft
nickel-based superalloy
|
|
gptkbp:first_flight
|
gptkb:1970
gptkb:1980
|
|
gptkbp:fuel_capacity
|
0.5 kg/shp/h
0.5 kg/s
180 kg/h
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
hydromechanical fuel control
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Turbomeca Arriel 1 E
|
|
gptkbp:ignition_system
|
spark ignition
dual ignition system
dual ignition
|
|
gptkbp:is_tested_for
|
ground testing required
|
|
gptkbp:launched
|
electric starter
starter-generator
|
|
gptkbp:length
|
1.2 m
1.1 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Turbomeca
|
|
gptkbp:noise_level
|
low
85 d B
|
|
gptkbp:number_of_stages
|
2
|
|
gptkbp:operational_range
|
up to 1000 km
|
|
gptkbp:power_output
|
500 shp
|
|
gptkbp:propulsion
|
3.5
4.2
4.2 shp/kg
|
|
gptkbp:service_ceiling
|
6000 m
|
|
gptkbp:services
|
gptkb:1980
|
|
gptkbp:successor
|
gptkb:Turbomeca_Arriel_2_B
|
|
gptkbp:torque
|
1500 Nm
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
helicopters
|
|
gptkbp:weight
|
120 kg
|