Statements (33)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Boeing_737_MAX
gptkb:Airbus_A320neo gptkb:COMAC_C919 |
| gptkbp:bypassRatio |
11:1
|
| gptkbp:certification |
gptkb:EASA
gptkb:FAA |
| gptkbp:countryOfOrigin |
gptkb:France
gptkb:United_States |
| gptkbp:familyMember |
gptkb:LEAP-1A
gptkb:LEAP-1B gptkb:LEAP-1C |
| gptkbp:firstFlight |
2014
|
| https://www.w3.org/2000/01/rdf-schema#label |
CFM LEAP
|
| gptkbp:introduced |
2016
|
| gptkbp:mainRotorDiameter |
78 inches
|
| gptkbp:manufacturer |
gptkb:CFM_International
|
| gptkbp:notableFeature |
fuel efficiency
reduced emissions composite fan blades lower noise ceramic matrix composite shrouds |
| gptkbp:predecessor |
gptkb:CFM56
|
| gptkbp:primaryUse |
narrow-body airliners
|
| gptkbp:thrust |
15,000–35,000 lbf
|
| gptkbp:usedBy |
gptkb:Boeing
gptkb:COMAC gptkb:Airbus |
| gptkbp:website |
https://www.cfmaeroengines.com/leap/
|
| gptkbp:bfsParent |
gptkb:CFM56
gptkb:CFM56_turbofan gptkb:CFM_LEAP-1A_(neo) |
| gptkbp:bfsLayer |
5
|