Statements (49)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:engine
|
| gptkbp:bfsLayer |
4
|
| gptkbp:bfsParent |
gptkb:CFM_International_LEAP-1_B
|
| gptkbp:aircraft_operated |
gptkb:aircraft
gptkb:Airbus_A320neo gptkb:Comac_C919 |
| gptkbp:application |
commercial aviation
|
| gptkbp:cancellation_reason |
up to 50% less noise
|
| gptkbp:design |
reduce fuel consumption
reduce noise footprint reduce C O2 emissions reduce N Ox emissions |
| gptkbp:diameter |
78 inches
|
| gptkbp:emissions_standard |
CAEP/6
|
| gptkbp:engine |
over 1,000
|
| gptkbp:engine_type |
gptkb:engine
|
| gptkbp:first_flight |
gptkb:2016
|
| gptkbp:fuel_capacity |
15% better than previous generation
|
| gptkbp:fuel_type |
lean burn combustor
|
| gptkbp:has_programs |
LEAP-X
|
| https://www.w3.org/2000/01/rdf-schema#label |
LEAP engine family
|
| gptkbp:key |
gptkb:film_production_company
advanced aerodynamics modular design reduced maintenance costs lightweight design enhanced durability reduced environmental impact high bypass ratio high thrust-to-weight ratio ceramic matrix composites real-time monitoring capabilities digital engine control sustainable aviation fuel compatibility advanced diagnostics systems modular maintenance approach advanced sealing technology high efficiency fan blades 3 D-printed fuel nozzle optimized for short-haul and long-haul flights high-pressure compressor technology improved performance at high altitudes low-pressure turbine technology |
| gptkbp:maintenance |
up to 30,000 hours
|
| gptkbp:manufacturer |
gptkb:CFM_International
|
| gptkbp:propulsion |
24,000 to 35,000 lbf
|
| gptkbp:services |
gptkb:2016
|
| gptkbp:technology |
advanced materials
|
| gptkbp:weight |
approximately 3,000 lbs
|