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gptkbp:instance_of
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gptkb:engine
|
|
gptkbp:bfsLayer
|
6
|
|
gptkbp:bfsParent
|
gptkb:Turbomeca_Arriel_1_B
|
|
gptkbp:accessories
|
gptkb:musician
gptkb:Company
gptkb:earthquake
gptkb:military_base
gptkb:engine
control unit
pressure sensor
mounting hardware
oil cooler
fuel system components
engine monitoring system
fuel control unit
fuel flow meter
starter generator
oil system components
engine control panel
power turbine governor
vibration sensor
exhaust system components
air system components
ignition unit
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|
gptkbp:application
|
gptkb:Bell_407
A S350 Écureuil
Eurocopter E C120 Colibri
|
|
gptkbp:average_temperature
|
-40 to 50 ° C
|
|
gptkbp:ceo
|
3,500 hours
|
|
gptkbp:compression_ratio
|
16:1
|
|
gptkbp:controls
|
gptkb:football_match
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
0.4 m
|
|
gptkbp:emissions_standard
|
ICAO Chapter 4
|
|
gptkbp:engine
|
free turbine
flexible mount
|
|
gptkbp:engine_type
|
axial compressor
single-stage turbine
|
|
gptkbp:first_flight
|
gptkb:1970
|
|
gptkbp:fuel_capacity
|
180 L/h
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
annular combustor
hydromechanical fuel control system
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Turbomeca Arriel 1 C
|
|
gptkbp:ignition_system
|
dual ignition system
|
|
gptkbp:launched
|
electric starter
|
|
gptkbp:length
|
1.1 m
|
|
gptkbp:maintenance
|
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Turbomeca
|
|
gptkbp:max_speed
|
42,000
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:number_of_stages
|
2
|
|
gptkbp:power_output
|
500 shp
|
|
gptkbp:propulsion
|
4.17 shp/kg
|
|
gptkbp:service_ceiling
|
3,000 m
|
|
gptkbp:type
|
gptkb:engine
|
|
gptkbp:used_in
|
helicopters
|
|
gptkbp:weight
|
120 kg
|