|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
business aviation
|
|
gptkbp:average_temperature
|
1,600 ° C
|
|
gptkbp:certification
|
EASA and FAA certified
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
high bypass turbofan
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
advanced cooling techniques
|
|
gptkbp:customer_support
|
gptkb:Bombardier_Global_7500
|
|
gptkbp:diameter
|
36 in
105 cm
|
|
gptkbp:emissions_standard
|
CAEP/8
|
|
gptkbp:engine
|
gptkb:business_jet
advanced aerodynamics
cutting-edge technology
in production
global market
ongoing development
global support network
3 D-printed components
blisk technology
|
|
gptkbp:engine_competitors
|
gptkb:General_Electric
|
|
gptkbp:engine_configuration
|
sustainability
advanced materials
twin-spool
|
|
gptkbp:engine_design_goal
|
reduce emissions
|
|
gptkbp:engine_launch_year
|
gptkb:2016
|
|
gptkbp:engine_materials
|
lightweight materials
|
|
gptkbp:engine_power
|
high reliability
high efficiency
high fuel efficiency
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
gptkb:Pearl_15
|
|
gptkbp:first_flight
|
gptkb:2018
|
|
gptkbp:fuel_capacity
|
1,200 lb
90 in
36 in
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Pearl 10 X
|
|
gptkbp:is_tested_for
|
extensive testing
|
|
gptkbp:length
|
90 in
|
|
gptkbp:maintenance
|
5,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Ford_Motor_Company
|
|
gptkbp:market_segment
|
ultra-long-range jets
|
|
gptkbp:noise_level
|
gptkb:Stage_5
low noise
|
|
gptkbp:power_source
|
Rolls-Royce Pearl series
|
|
gptkbp:propulsion
|
10,000 lbf
8.33
|
|
gptkbp:service_ceiling
|
51,000 ft
|
|
gptkbp:turbine_type
|
high-pressure turbine
|
|
gptkbp:weight
|
1,200 lb
|
|
gptkbp:bfsParent
|
gptkb:Dassault_Falcon_10_X
|
|
gptkbp:bfsLayer
|
6
|