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gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:aircraft_operated
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gptkb:Airbus_A320neo
gptkb:Boeing_737
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gptkbp:application
|
commercial aviation
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gptkbp:cancellation_reason
|
significantly reduced noise levels
|
|
gptkbp:combustor_type
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advanced ceramic matrix composites
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gptkbp:competitors
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gptkb:Pratt_&_Whitney_PW1100_G
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gptkbp:control_system
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gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
advanced cooling techniques
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|
gptkbp:customer_base
|
airlines worldwide
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gptkbp:design
|
high bypass ratio
|
|
gptkbp:diameter
|
78 inches
|
|
gptkbp:emissions_standard
|
lower NOx emissions than previous engines
|
|
gptkbp:engine
|
gptkb:LEAP_engine_family
|
|
gptkbp:first_flight
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gptkb:2016
|
|
gptkbp:fuel_economy
|
15% better than previous engines
|
|
gptkbp:has_programs
|
LEAP program
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
General Electric LEAP
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|
gptkbp:maintenance
|
higher than previous models
|
|
gptkbp:manufacturer
|
gptkb:General_Electric
|
|
gptkbp:operational_use
|
high altitude and high speed
|
|
gptkbp:partnership
|
gptkb:Safran_Aircraft_Engines
|
|
gptkbp:propulsion
|
24,000 to 33,000 lbf
|
|
gptkbp:service_entry
|
gptkb:2016
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:weight
|
approximately 3,000 lbs
|
|
gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_Pure_Power_family
|
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gptkbp:bfsLayer
|
8
|