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gptkbp:instance_of
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gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:Airbus_A320neo
gptkb:Boeing_737
gptkb:Comac_C919
|
|
gptkbp:average_temperature
|
up to 1,600° F
|
|
gptkbp:bypass_ratio
|
9:1
|
|
gptkbp:cancellation_reason
|
up to 50% less than CFM56
|
|
gptkbp:certification
|
FAA certified
EASA certified
|
|
gptkbp:combustor_type
|
lean burn combustor
|
|
gptkbp:customer_support
|
GE Aviation's global network
|
|
gptkbp:development
|
gptkb:MTU_Aero_Engines
gptkb:Safran_Aircraft_Engines
|
|
gptkbp:diameter
|
78 inches
|
|
gptkbp:emissions_standard
|
lower NOx emissions than CAEP/6 standards
|
|
gptkbp:environmental_impact
|
lower carbon footprint
|
|
gptkbp:first_flight
|
gptkb:2016
|
|
gptkbp:fuel_economy
|
15% better than CFM56
reduced fuel consumption
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
LEAP Engine
|
|
gptkbp:innovation
|
advanced materials
modular architecture
|
|
gptkbp:launch_date
|
gptkb:2014
|
|
gptkbp:maintenance
|
up to 30% longer than CFM56
|
|
gptkbp:manufacturer
|
gptkb:GE_Aviation
|
|
gptkbp:market_share
|
leading engine in narrowbody segment
|
|
gptkbp:partnerships
|
gptkb:Airbus
gptkb:Boeing
Comac
|
|
gptkbp:performance
|
high thrust-to-weight ratio
|
|
gptkbp:project
|
gptkb:LEAP-1_A
gptkb:LEAP-1_B
gptkb:LEAP-1_C
|
|
gptkbp:propulsion
|
up to 35,000 lbf
|
|
gptkbp:service
|
up to 30,000 hours
|
|
gptkbp:technology
|
advanced aerodynamics
composite fan blades
3 D-printed fuel nozzle
|
|
gptkbp:total_deliveries
|
over 7,000
|
|
gptkbp:total_orders
|
over 17,000
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:weight
|
approximately 3,000 lbs
|
|
gptkbp:bfsParent
|
gptkb:GE_Aviation
|
|
gptkbp:bfsLayer
|
4
|