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gptkbp:instance_of
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gptkb:jet_engine
|
|
gptkbp:application
|
business aviation
|
|
gptkbp:certification
|
EASA and FAA
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:competitors
|
gptkb:Pratt_&_Whitney_Canada_PW535_E
|
|
gptkbp:compressor_type
|
gptkb:6
|
|
gptkbp:control_system
|
gptkb:Full_Authority_Digital_Engine_Control_(FADEC)
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:customer_support
|
gptkb:Bombardier_Global_5500
|
|
gptkbp:design_feature
|
low noise
|
|
gptkbp:diameter
|
28 inches
36 inches
|
|
gptkbp:emissions_standard
|
CAEP/8
|
|
gptkbp:engine
|
gptkb:Pearl_family
gptkb:business_jet
high bypass ratio
future upgrade potential
advanced noise reduction technology
state-of-the-art materials
business aviation market
comprehensive customer support services
next-generation engine technology
collaborative development process
|
|
gptkbp:engine_configuration
|
advanced aerodynamics
twin-engine
sustainability-focused
5000 lbf
|
|
gptkbp:engine_power
|
high reliability
optimized for efficiency
|
|
gptkbp:engine_type
|
turbofan
|
|
gptkbp:first_flight
|
gptkb:2018
|
|
gptkbp:fuel_capacity
|
60 inches
3000 lb
36 inches
|
|
gptkbp:fuel_economy
|
high
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Rolls-Royce Pearl 500
|
|
gptkbp:is_tested_for
|
extensive ground and flight testing
|
|
gptkbp:launch_date
|
gptkb:2018
|
|
gptkbp:length
|
approximately 60 inches
|
|
gptkbp:maintenance
|
5000 hours
|
|
gptkbp:manufacturer
|
gptkb:Ford_Motor_Company
|
|
gptkbp:market_segment
|
ultra-long-range jets
|
|
gptkbp:max_speed
|
Mach 0.85
|
|
gptkbp:noise_level
|
gptkb:Stage_5
|
|
gptkbp:propulsion
|
5000 lbf
1.67
|
|
gptkbp:service_ceiling
|
45,000 feet
|
|
gptkbp:technology
|
geared turbofan
|
|
gptkbp:turbine_type
|
2
|
|
gptkbp:weight
|
approximately 3000 lb
|
|
gptkbp:bfsParent
|
gptkb:Rolls-Royce_Pearl_700
|
|
gptkbp:bfsLayer
|
6
|