Statements (29)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bypassRatio |
11:1
|
| gptkbp:certification |
gptkb:EASA
gptkb:FAA |
| gptkbp:competitor |
gptkb:Pratt_&_Whitney_PW1000G
|
| gptkbp:countryOfOrigin |
gptkb:France
gptkb:United_States |
| gptkbp:enteredService |
2016
|
| gptkbp:features |
3D-printed fuel nozzles
ceramic matrix composites composite fan blades |
| gptkbp:firstFlight |
2014
|
| gptkbp:hasConcept |
high-bypass turbofan
|
| https://www.w3.org/2000/01/rdf-schema#label |
CFM International LEAP
|
| gptkbp:intendedUse |
narrow-body aircraft
|
| gptkbp:mainRotorDiameter |
78 inches
|
| gptkbp:manufacturer |
gptkb:CFM_International
|
| gptkbp:notableOperation |
gptkb:Southwest_Airlines
gptkb:Boeing gptkb:Airbus |
| gptkbp:partner |
gptkb:GE_Aviation
gptkb:Safran_Aircraft_Engines |
| gptkbp:predecessor |
gptkb:CFM56
|
| gptkbp:thrust |
23,000–35,000 lbf
|
| gptkbp:usedOn |
gptkb:Boeing_737_MAX
gptkb:Airbus_A320neo gptkb:COMAC_C919 |
| gptkbp:bfsParent |
gptkb:CFM_International_LEAP-1B
|
| gptkbp:bfsLayer |
5
|