Statements (27)
Predicate | Object |
---|---|
gptkbp:instance_of |
gptkb:turbofan_engine
|
gptkbp:application |
gptkb:Airbus
|
gptkbp:armament |
24 fan blades
|
gptkbp:bypass_ratio |
4.5:1
|
gptkbp:combustor_type |
annular combustor
|
gptkbp:compressor_type |
axial compressor
|
gptkbp:control_system |
gptkb:full_authority_digital_engine_control_(FADEC)
|
gptkbp:cooling_system |
air-cooled
|
gptkbp:diameter |
1.5 m
|
gptkbp:emissions_standard |
ICAO Chapter 4
|
gptkbp:fuel_type |
gptkb:Jet_A
|
gptkbp:gearbox |
reduction gearbox
|
https://www.w3.org/2000/01/rdf-schema#label |
V2500-E5
|
gptkbp:maintenance |
4,000 hours
|
gptkbp:manufacturer |
gptkb:International_Aero_Engines
|
gptkbp:noise_level |
Stage 3 compliant
|
gptkbp:operational_range |
-54 to 50 ° C
|
gptkbp:original_run |
gptkb:1988
|
gptkbp:produces |
over 6,000 engines
|
gptkbp:propulsion |
25,000 lbf
|
gptkbp:service_entry |
gptkb:1997
|
gptkbp:turbine_type |
high-pressure turbine
|
gptkbp:type |
high-bypass turbofan
|
gptkbp:weight |
3,000 lb
|
gptkbp:bfsParent |
gptkb:V2500
gptkb:IAE_V2500 |
gptkbp:bfsLayer |
5
|