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gptkbp:instance_of
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gptkb:jet_engine
|
|
gptkbp:application
|
commercial aviation
|
|
gptkbp:average_temperature
|
higher operating temperatures
|
|
gptkbp:bypass_ratio
|
9:1
|
|
gptkbp:cancellation_reason
|
significantly reduced noise footprint
|
|
gptkbp:certification
|
FAA certified
EASA certified
|
|
gptkbp:combustor_type
|
lean burn combustor
|
|
gptkbp:cooling_system
|
advanced cooling technology
|
|
gptkbp:customer_base
|
over 100 customers
|
|
gptkbp:customer_feedback
|
incorporated customer feedback into design.
|
|
gptkbp:customer_support
|
gptkb:Air_France
comprehensive customer support
|
|
gptkbp:design
|
collaborative design team
30,000 flight hours
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:diameter
|
78 inches
|
|
gptkbp:emissions_standard
|
lower CO2 emissions
|
|
gptkbp:engine
|
part of LEAP engine family
|
|
gptkbp:engine_configuration
|
twin-spool configuration
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
|
|
gptkbp:environmental_impact
|
reduced environmental impact
|
|
gptkbp:first_flight
|
gptkb:2016
|
|
gptkbp:fuel_economy
|
15% better than CFM56
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
gptkbp:has_programs
|
gptkb:LEAP_engine_family
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CFM LEAP-1 A engine
|
|
gptkbp:innovation
|
digital engine control system
|
|
gptkbp:legal_principle
|
gptkb:jet_engine
|
|
gptkbp:maintenance
|
longer maintenance intervals
|
|
gptkbp:manufacturer
|
gptkb:CFM_International
|
|
gptkbp:market_segment
|
narrow-body aircraft
|
|
gptkbp:market_share
|
dominant market share in its class
|
|
gptkbp:network
|
global support network
|
|
gptkbp:operational_cost
|
lower operational costs
|
|
gptkbp:operational_period
|
high bypass ratio cycle
|
|
gptkbp:partnerships
|
strategic partnerships with airlines
|
|
gptkbp:project
|
ongoing future developments
|
|
gptkbp:propulsion
|
up to 35,000 lbf
|
|
gptkbp:rating
|
high performance rating
|
|
gptkbp:related_aircraft
|
gptkb:Airbus_A320neo
gptkb:COMAC_C919
gptkb:Boeing_737
|
|
gptkbp:research_and_development
|
extensive research and development efforts
|
|
gptkbp:rival_engine
|
gptkb:Rolls-Royce_Trent_1000
gptkb:Pratt_&_Whitney_PW1100_G
|
|
gptkbp:service_entry
|
gptkb:2016
|
|
gptkbp:squadrons
|
over 1,000 engines in service
|
|
gptkbp:sustainability
|
focus on sustainability
|
|
gptkbp:technology
|
advanced materials
3 D-printed fuel nozzle
|
|
gptkbp:weight
|
lighter than previous models
|
|
gptkbp:bfsParent
|
gptkb:Snecma_Propulsion
|
|
gptkbp:bfsLayer
|
6
|