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gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:air_support
|
optimized airflow design
|
|
gptkbp:application
|
commercial aviation
narrow-body aircraft
|
|
gptkbp:armament
|
gptkb:textiles
carbon fiber composite
|
|
gptkbp:bypass_ratio
|
9:1
|
|
gptkbp:cancellation_reason
|
50% quieter than CFM56
up to 50% compared to CFM56
|
|
gptkbp:certification
|
FAA certification
FAA certified
|
|
gptkbp:combustor_type
|
lean burn combustor
|
|
gptkbp:competitors
|
gptkb:Pratt_&_Whitney_GTF
gptkb:Pratt_&_Whitney_PW1100_G
|
|
gptkbp:compressor_type
|
high-pressure compressor with 10 stages
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
advanced cooling technology
|
|
gptkbp:customer_base
|
global airlines
|
|
gptkbp:customer_support
|
gptkb:Boeing
global support network
|
|
gptkbp:design
|
30,000 cycles
|
|
gptkbp:design_purpose
|
fuel efficiency
|
|
gptkbp:development
|
gptkb:GE_Aviation
|
|
gptkbp:diameter
|
68 inches
|
|
gptkbp:emissions_standard
|
lower NOx emissions
|
|
gptkbp:engine
|
gptkb:LEAP_engine_family
advanced aerodynamics
modular design
ongoing research and development
continuous innovation
|
|
gptkbp:engine_configuration
|
upgradeable design
|
|
gptkbp:engine_lifecycle_costs
|
low lifecycle costs
|
|
gptkbp:engine_maintenance_costs
|
competitive maintenance costs
|
|
gptkbp:engine_nozzle
|
variable area nozzle
|
|
gptkbp:engine_optimization
|
optimized for efficiency
|
|
gptkbp:engine_performance_metrics
|
meets performance metrics
|
|
gptkbp:engine_power
|
high thermal efficiency
high reliability rating
|
|
gptkbp:engine_shutdown
|
smooth shutdown process
|
|
gptkbp:engine_startup
|
quick startup time
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
compatible with various aircraft systems
|
|
gptkbp:first_flight
|
gptkb:2016
|
|
gptkbp:fuel_capacity
|
approximately 11.5 feet
approximately 2.5 feet
|
|
gptkbp:fuel_economy
|
15% better than CFM56
|
|
gptkbp:fuel_type
|
Jet A or Jet A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
CFM International LEAP-1 B
|
|
gptkbp:inspiration
|
reduce fuel consumption
|
|
gptkbp:is_tested_for
|
extensive testing program
|
|
gptkbp:maintenance
|
8,000 hours
|
|
gptkbp:manufacturer
|
gptkb:CFM_International
|
|
gptkbp:market_share
|
dominant in narrow-body segment
|
|
gptkbp:material
|
composite fan blades
|
|
gptkbp:noise_level
|
low noise levels
|
|
gptkbp:operational_period
|
high bypass ratio
high bypass turbofan engine
|
|
gptkbp:operational_use
|
commercial aviation
|
|
gptkbp:order
|
over 15,000 engines
|
|
gptkbp:original_run
|
gptkb:2016
|
|
gptkbp:performance
|
high performance engine
|
|
gptkbp:propulsion
|
26,000 to 29,000 lbf
|
|
gptkbp:related_aircraft
|
gptkb:Boeing_737_family
|
|
gptkbp:service_entry
|
gptkb:2017
|
|
gptkbp:sustainability
|
designed for lower environmental impact
|
|
gptkbp:technology
|
LEAP engine technology
|
|
gptkbp:total_orders
|
over 15,000 engines
|
|
gptkbp:turbine_type
|
high-pressure turbine
high-pressure turbine with 2 stages
|
|
gptkbp:used_in
|
gptkb:Boeing_737
|
|
gptkbp:weight
|
approximately 3,000 lbs
3,000 lb
|
|
gptkbp:weight_savings
|
lightweight design
|
|
gptkbp:bfsParent
|
gptkb:Boeing_P-8_Poseidon
gptkb:Boeing_737_MAX_9
gptkb:737_MAX_10
gptkb:Boeing_737_MAX_8
gptkb:Boeing_737
gptkb:Boeing_737_MAX_10
gptkb:Boeing_737_MAX_7
gptkb:737_MAX
|
|
gptkbp:bfsLayer
|
5
|