Statements (31)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
commercial aviation
|
| gptkbp:bypassRatio |
9:1
|
| gptkbp:certification |
May 2016
|
| gptkbp:countryOfOrigin |
gptkb:France
gptkb:United_States |
| gptkbp:developedBy |
gptkb:CFM_International
|
| gptkbp:family |
gptkb:LEAP_engine_family
|
| gptkbp:firstFlight |
2016
|
| gptkbp:fuelEfficiencyImprovement |
15% over CFM56-7B
|
| gptkbp:hasConcept |
high-bypass turbofan
|
| https://www.w3.org/2000/01/rdf-schema#label |
LEAP-1B
|
| gptkbp:length |
78.5 inches
|
| gptkbp:mainRotorDiameter |
69.4 inches
|
| gptkbp:manufacturer |
gptkb:CFM_International
|
| gptkbp:notableFeature |
lower emissions
composite fan blades lower noise reduced fuel consumption ceramic matrix composite parts |
| gptkbp:numberOfStages |
2
10 |
| gptkbp:primaryUser |
gptkb:Boeing
|
| gptkbp:replacedBy |
gptkb:CFM56-7B
|
| gptkbp:thrust |
23,000–28,000 lbf
|
| gptkbp:usedOn |
gptkb:Boeing_737_MAX
|
| gptkbp:weight |
6,129 lb
|
| gptkbp:bfsParent |
gptkb:B737
gptkb:CFM56-7B gptkb:CFM_LEAP-1A_(neo) |
| gptkbp:bfsLayer |
5
|