Statements (27)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
narrow-body airliners
|
| gptkbp:bypassRatio |
9:1
|
| gptkbp:certification |
2017
|
| gptkbp:countryOfOrigin |
gptkb:France
gptkb:United_States |
| gptkbp:diameter |
78 inches
|
| gptkbp:features |
composite fan blades
advanced fuel efficiency ceramic matrix composite parts |
| gptkbp:firstRun |
2013
|
| gptkbp:hasConcept |
high-bypass
|
| https://www.w3.org/2000/01/rdf-schema#label |
LEAP-1C
|
| gptkbp:length |
78 inches
|
| gptkbp:mainRotorDiameter |
78 inches
|
| gptkbp:manufacturer |
gptkb:CFM_International
|
| gptkbp:marketEntry |
2017
|
| gptkbp:notableFor |
first engine with integrated propulsion system for C919
|
| gptkbp:parentCompany |
gptkb:GE_Aviation
gptkb:Safran_Aircraft_Engines |
| gptkbp:relatedTo |
gptkb:LEAP-1A
gptkb:LEAP-1B |
| gptkbp:thrust |
27,980 lbf
|
| gptkbp:usedOn |
gptkb:Comac_C919
|
| gptkbp:weight |
2,900 lb
|
| gptkbp:bfsParent |
gptkb:CFM_LEAP-1A_(neo)
|
| gptkbp:bfsLayer |
5
|