Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turbofan engine family
|
| gptkbp:bypassRatio |
11:1
|
| gptkbp:certification |
2016
|
| gptkbp:countryOfOrigin |
gptkb:France
gptkb:United_States |
| gptkbp:emissionsReduction |
50% NOx reduction compared to CAEP/6
|
| gptkbp:firstFlight |
2014
|
| gptkbp:fuelEfficiencyImprovement |
15% over CFM56
|
| https://www.w3.org/2000/01/rdf-schema#label |
LEAP engine family
|
| gptkbp:intendedAircraft |
gptkb:Boeing_737_MAX
gptkb:Airbus_A320neo gptkb:COMAC_C919 |
| gptkbp:manufacturer |
gptkb:CFM_International
|
| gptkbp:noiseReduction |
15 dB lower than CFM56
|
| gptkbp:predecessor |
gptkb:CFM56
|
| gptkbp:primaryUser |
gptkb:Boeing
gptkb:COMAC gptkb:Airbus |
| gptkbp:technology |
3D-printed fuel nozzles
ceramic matrix composites composite fan blades |
| gptkbp:thrust |
15,000–35,000 lbf
|
| gptkbp:variant |
gptkb:LEAP-1A
gptkb:LEAP-1B gptkb:LEAP-1C |
| gptkbp:bfsParent |
gptkb:LEAP-1B
|
| gptkbp:bfsLayer |
6
|