|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:aircraft_operated
|
gptkb:Bombardier_Global_7500
|
|
gptkbp:application
|
business aviation
|
|
gptkbp:cancellation_reason
|
yes
|
|
gptkbp:certification
|
FAA certified
EASA certified
EASA and FAA
|
|
gptkbp:compressor_type
|
axial
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
modular design
|
|
gptkbp:diameter
|
1,000 mm
|
|
gptkbp:emissions_standard
|
CAEP/6
|
|
gptkbp:engine
|
advanced aerodynamics
state-of-the-art technology
extensive research and development
global support network
next-generation technology
business aircraft
part of Rolls-Royce legacy
|
|
gptkbp:engine_configuration
|
innovative design
twin-spool
|
|
gptkbp:engine_materials
|
advanced composites
|
|
gptkbp:engine_power
|
high reliability
high efficiency
superior performance
|
|
gptkbp:engine_type
|
gptkb:business_jet
turbofan
|
|
gptkbp:engine_upgrades
|
future upgrades possible
|
|
gptkbp:first_flight
|
gptkb:2016
|
|
gptkbp:fuel_capacity
|
1,000 mm
2,500 mm
300 kg
|
|
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 15
|
|
gptkbp:launch_date
|
gptkb:2016
|
|
gptkbp:length
|
2,500 mm
|
|
gptkbp:maintenance
|
easy maintenance
5,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Ford_Motor_Company
|
|
gptkbp:market_segment
|
ultra-long-range jets
|
|
gptkbp:noise_level
|
low noise
low vibration
|
|
gptkbp:number_of_stages
|
gptkb:5
|
|
gptkbp:propulsion
|
15,000 lbf
|
|
gptkbp:service_entry
|
gptkb:2018
|
|
gptkbp:successor
|
gptkb:Rolls-Royce_BR710
|
|
gptkbp:turbine_inlet_temperature
|
1,600 ° C
|
|
gptkbp:turbine_type
|
high bypass ratio
|
|
gptkbp:weight
|
300 kg
|
|
gptkbp:bfsParent
|
gptkb:Bombardier_Global_Series
gptkb:Bombardier_Global_series
|
|
gptkbp:bfsLayer
|
5
|