Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
gptkb:Comac_C919
|
| gptkbp:bypassRatio |
9:1
|
| gptkbp:certification |
2017
|
| gptkbp:countryOfOrigin |
gptkb:France
gptkb:United_States |
| gptkbp:emissionsReduction |
15% lower CO2 than CFM56
|
| gptkbp:family |
gptkb:CFM_International_LEAP
|
| gptkbp:features |
ceramic matrix composites
composite fan blades advanced fuel efficiency |
| gptkbp:firstFlight |
2014
|
| gptkbp:hasConcept |
high-bypass
|
| https://www.w3.org/2000/01/rdf-schema#label |
CFM International LEAP-1C
|
| gptkbp:mainRotorDiameter |
78 inches
|
| gptkbp:manufacturer |
gptkb:CFM_International
|
| gptkbp:marketedAs |
single-aisle airliners
|
| gptkbp:noiseReduction |
compliant with ICAO Chapter 4
|
| gptkbp:predecessor |
gptkb:CFM56
|
| gptkbp:thrust |
27,980–31,000 lbf
|
| gptkbp:bfsParent |
gptkb:Comac_C919
|
| gptkbp:bfsLayer |
5
|