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gptkbp:instance_of
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gptkb:engine
|
|
gptkbp:bfsLayer
|
7
|
|
gptkbp:bfsParent
|
gptkb:Turbomeca_Arriel_1_E
gptkb:Sikorsky_S-76_helicopter
|
|
gptkbp:application
|
gptkb:Bell_407
A S350 Écureuil
Eurocopter E C120 Colibri
|
|
gptkbp:average_temperature
|
up to 700 ° C
|
|
gptkbp:certification
|
EASA certified
|
|
gptkbp:compression_ratio
|
16:1
|
|
gptkbp:controls
|
gptkb:football_match
digital electronic control
|
|
gptkbp:cooling_system
|
air
air-cooled
|
|
gptkbp:design
|
5000 hours
|
|
gptkbp:diameter
|
0.3 m
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissions_standard
|
single exhaust
ICAO Chapter 4
|
|
gptkbp:engine
|
free turbine
electric start
flexible mount
turbo-shaft
|
|
gptkbp:engine_type
|
gptkb:engine
single spool
nickel-based superalloy
ceramic matrix composite
|
|
gptkbp:first_flight
|
gptkb:1970
|
|
gptkbp:fuel_capacity
|
dry sump
180 kg/h
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
dual fuel system
engine-driven pump
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Turbomeca Arriel 1 S
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:launched
|
starter-generator
|
|
gptkbp:length
|
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
|
1000 km
|
|
gptkbp:power_output
|
500 shp
|
|
gptkbp:propulsion
|
not applicable
4.17 shp/kg
|
|
gptkbp:service_ceiling
|
5000 m
|
|
gptkbp:speed
|
42,000 rpm
|
|
gptkbp:torque
|
1500 Nm
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
helicopters
|
|
gptkbp:weight
|
120 kg
150 kg
|