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gptkbp:instance_of
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gptkb:jet_engine
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gptkbp:application
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regional jets
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gptkbp:armament
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gptkb:textiles
|
|
gptkbp:average_temperature
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1,500 ° C
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gptkbp:certification
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FAA certified
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gptkbp:combustor_type
|
annular combustor
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gptkbp:compressor_type
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axial compressor
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gptkbp:control_system
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gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
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gptkbp:cooling_system
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air-cooled
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gptkbp:design
|
20,000 hours
|
|
gptkbp:diameter
|
1.5 m
1.1 m
|
|
gptkbp:emissions_standard
|
low NOx
|
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gptkbp:engine_configuration
|
twin-spool
pylon mounted
high bypass ratio turbofan
|
|
gptkbp:exhaust_system
|
subsonic intake
|
|
gptkbp:first_flight
|
gptkb:1996
|
|
gptkbp:fuel_capacity
|
dry sump
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
gptkb:gasoline
electronic fuel control
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
AE 3007 engine
|
|
gptkbp:ignition_system
|
spark ignition
|
|
gptkbp:is_tested_for
|
static testing
|
|
gptkbp:launched
|
air starter
|
|
gptkbp:length
|
2.5 m
|
|
gptkbp:maintenance
|
5,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:market_segment
|
regional aviation
|
|
gptkbp:noise_level
|
Stage 4 compliant
|
|
gptkbp:number_of_stages
|
gptkb:10
|
|
gptkbp:operational_range
|
high altitude
|
|
gptkbp:operational_use
|
tropical and temperate climates
|
|
gptkbp:propulsion
|
gptkb:12.5
15,000 lbf
cascade type
|
|
gptkbp:service_entry
|
gptkb:1997
|
|
gptkbp:turbine_blades
|
single crystal alloy
|
|
gptkbp:turbine_type
|
high bypass ratio
|
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gptkbp:type
|
gptkb:turbofan_engine
|
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gptkbp:used_in
|
gptkb:Bombardier_Q-Series
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:Rolls-Royce_Defence
|
|
gptkbp:bfsLayer
|
5
|