Statements (28)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bypassRatio |
11:1
|
| gptkbp:certification |
2016
|
| gptkbp:countryOfOrigin |
gptkb:France
gptkb:United_States |
| gptkbp:features |
3D-printed fuel nozzles
ceramic matrix composites composite fan blades |
| gptkbp:firstFlight |
2014
|
| gptkbp:hasVariant |
gptkb:LEAP-1A
gptkb:LEAP-1B gptkb:LEAP-1C |
| https://www.w3.org/2000/01/rdf-schema#label |
LEAP engine
|
| gptkbp:intendedUse |
narrow-body aircraft
|
| gptkbp:mainRotorDiameter |
78 inches
|
| gptkbp:manufacturer |
gptkb:CFM_International
|
| gptkbp:operator |
gptkb:Boeing
gptkb:COMAC gptkb:Airbus |
| gptkbp:parentCompany |
gptkb:GE_Aviation
gptkb:Safran_Aircraft_Engines |
| gptkbp:predecessor |
gptkb:CFM56
|
| gptkbp:thrust |
23,000–35,000 lbf
|
| gptkbp:usedOn |
gptkb:Airbus_A320neo_family
gptkb:Boeing_737_MAX gptkb:COMAC_C919 |
| gptkbp:bfsParent |
gptkb:GE_Aerospace
|
| gptkbp:bfsLayer |
5
|