Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
4
|
| gptkbp:bfsParent |
gptkb:V2500
gptkb:IAE_V2500 |
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:armament |
24 fan blades
|
| gptkbp:bypass_ratio |
4.5:1
|
| gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
| gptkbp:cooling_system |
air-cooled
|
| gptkbp:diameter |
1.5 m
|
| gptkbp:drivetrain |
reduction gearbox
|
| gptkbp:emissions_standard |
ICAO Chapter 4
|
| gptkbp:engine_type |
axial compressor
high-pressure turbine |
| gptkbp:fuel_type |
gptkb:Jet_A
annular combustor |
| 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:produced_by |
over 6,000 engines
|
| gptkbp:propulsion |
25,000 lbf
|
| gptkbp:services |
gptkb:1997
|
| gptkbp:type |
high-bypass turbofan
|
| gptkbp:weight |
3,000 lb
|