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gptkbp:instance_of
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gptkb:jet_engine
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|
gptkbp:application
|
gptkb:business_jet
|
|
gptkbp:average_temperature
|
up to 2000 ° F
|
|
gptkbp:certification
|
FAA certified
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|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
|
|
gptkbp:cooling_system
|
air-cooled
interstage cooling
|
|
gptkbp:development
|
Rolls-Royce BR700 family
|
|
gptkbp:diameter
|
approximately 1.5 m
approximately 1.2 m
|
|
gptkbp:emissions_certification
|
CAEP/6
|
|
gptkbp:engine
|
commercial aviation
state-of-the-art technology
innovative design
quiet operation
|
|
gptkbp:engine_category
|
business aviation
|
|
gptkbp:engine_configuration
|
wing-mounted
advanced design
|
|
gptkbp:engine_power
|
high reliability
optimized performance
long lifecycle
|
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gptkbp:engine_type
|
compatible with various aircraft.
|
|
gptkbp:first_flight
|
gptkb:2001
|
|
gptkbp:fuel_economy
|
high efficiency
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
BR710 A2-40
|
|
gptkbp:is_tested_for
|
extensive testing
|
|
gptkbp:length
|
approximately 3.5 m
|
|
gptkbp:maintenance
|
5000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:noise_level
|
gptkb:Stage_4
|
|
gptkbp:notable_users
|
gptkb:Dassault_Falcon_7_X
gptkb:Gulfstream_G650
gptkb:Bombardier_Global_Express
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:number_of_stages
|
10 stages
|
|
gptkbp:propulsion
|
no
70 k N
|
|
gptkbp:service_entry
|
gptkb:2003
|
|
gptkbp:starting_system
|
air start
|
|
gptkbp:turbine_type
|
high bypass ratio turbine
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:weight
|
approximately 2000 lbs
|
|
gptkbp:bfsParent
|
gptkb:Rolls-Royce_BR710
|
|
gptkbp:bfsLayer
|
5
|