Statements (93)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:turbofan_engine
|
| gptkbp:application |
gptkb:helicopter
helicopters |
| gptkbp:average_temperature |
high temperature
|
| gptkbp:certification |
EASA certified
certified by authorities |
| gptkbp:combustor_type |
annular
annular combustion chamber |
| gptkbp:compression_ratio |
10:1
|
| gptkbp:compressor_type |
axial compressor
|
| gptkbp:control_system |
digital control system
electronic control system |
| gptkbp:cooling_system |
air-cooled
direct air cooling |
| gptkbp:design |
modular design
|
| gptkbp:design_date |
1960s
|
| gptkbp:diameter |
0.4 m
|
| gptkbp:emissions_standard |
low emissions
compliant with ICAO standards |
| gptkbp:engine |
gptkb:Turbomeca_Arriel
gptkb:civil_aviation gptkb:advanced_technology compact design continuous improvement initiatives innovative design ongoing development global support network turbo-shaft technical support provided factory assembled proven legacy starter motor advanced turbine technology long-standing operational history |
| gptkbp:engine_category |
civil and military use
|
| gptkbp:engine_configuration |
upgrade options available
upgrade options single engine single spool single shaft flexible mounting system |
| gptkbp:engine_distribution |
global distribution network
|
| gptkbp:engine_power |
high performance
high reliability high efficiency 2000 hours high reliability rating up to 5,000 hours excellent performance metrics |
| gptkbp:engine_shutdown |
smooth shutdown
|
| gptkbp:engine_startup |
quick startup
|
| gptkbp:engine_type |
gptkb:turbofan_engine
compatible with various airframes various airframes |
| gptkbp:exhaust_system |
axial
free turbine |
| gptkbp:first_flight |
gptkb:1960
|
| gptkbp:fuel_capacity |
150 kg
|
| gptkbp:fuel_economy |
200 kg/h
0.5 kg/k W/h |
| gptkbp:fuel_type |
gptkb:Jet_A-1
|
| gptkbp:gearbox |
reduction gearbox
|
| https://www.w3.org/2000/01/rdf-schema#label |
Turbomeca Astazou IIIB
|
| gptkbp:is_tested_for |
ground testing required
|
| gptkbp:launch_window |
starter-generator
|
| gptkbp:length |
1.2 m
|
| gptkbp:maintenance |
scheduled maintenance
500 hours overhaul services available |
| gptkbp:manufacturer |
gptkb:Turbomeca
|
| gptkbp:noise_level |
low
quiet operation low vibration low noise emissions |
| gptkbp:notable_users |
gptkb:Aérospatiale_SA_330_Puma
gptkb:Eurocopter_AS350_Écureuil Aérospatiale SA 315 B Lama |
| gptkbp:number_of_stages |
2
|
| gptkbp:operational_range |
varied
up to 30,000 ft |
| gptkbp:operational_use |
military and civilian aircraft
|
| gptkbp:power_output |
370 k W
480 k W |
| gptkbp:powers |
3.1 k W/kg
|
| gptkbp:propulsion |
650 shp
500 lbf |
| gptkbp:service_ceiling |
up to 20,000 ft
|
| gptkbp:successor |
Turbomeca Astazou IIIC
|
| gptkbp:turbine_type |
free power turbine
|
| gptkbp:type |
gptkb:turbofan_engine
|
| gptkbp:used_in |
gptkb:Aérospatiale_SA_315_Lama
|
| gptkbp:weight |
120 kg
150 kg |