|
gptkbp:instance_of
|
gptkb:engine
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:Arriel_2_B
gptkb:Arriel_engine
|
|
gptkbp:application
|
gptkb:aircraft
|
|
gptkbp:average_temperature
|
-40 to 50 ° C
900 ° C
|
|
gptkbp:certification
|
EASA certified
|
|
gptkbp:compression_ratio
|
16:1
|
|
gptkbp:controls
|
gptkb:football_match
digital control system
|
|
gptkbp:cooling_system
|
gptkb:engine
air-cooled
|
|
gptkbp:design
|
5000 hours
|
|
gptkbp:diameter
|
0.5 m
|
|
gptkbp:drivetrain
|
reduction gearbox
|
|
gptkbp:emissions_standard
|
ICAO Chapter 4
|
|
gptkbp:engine
|
Brayton cycle
twin-spool
horizontal layout
Arriel family
|
|
gptkbp:engine_type
|
gptkb:engine
axial compressor
single-stage turbine
two stages
single stage
Arriel 2 series
|
|
gptkbp:fuel_capacity
|
0.5 kg/s
0.5 kg/k W·h
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
dual fuel system
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Arriel 2 C
|
|
gptkbp:ignition_system
|
electronic ignition
|
|
gptkbp:investment
|
30 psi
|
|
gptkbp:launched
|
starter-generator
|
|
gptkbp:length
|
1.2 m
|
|
gptkbp:lens_type
|
flexible mount
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Safran_Helicopter_Engines
|
|
gptkbp:max_speed
|
40,000 rpm
60,000 rpm
|
|
gptkbp:noise_level
|
low
85 d B
|
|
gptkbp:number_of_stages
|
2
|
|
gptkbp:original_run
|
gptkb:1980s
|
|
gptkbp:power_output
|
480 k W
|
|
gptkbp:propulsion
|
650 shp
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
20,000 ft
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
Eurocopter A S350
|
|
gptkbp:water_source
|
replaceable
|
|
gptkbp:weight
|
150 kg
200 kg
|