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gptkbp:instanceOf
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engine
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gptkbp:aircraft
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gptkb:Embraer_ERJ_140
gptkb:Embraer_ERJ_135
Bombardier CRJ-200
|
|
gptkbp:application
|
Regional_Jets
|
|
gptkbp:certifications
|
gptkb:FAA
|
|
gptkbp:compressionRatio
|
24:1
5:1
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|
gptkbp:controls
|
Electronic control system
|
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gptkbp:coolingSystem
|
Air-cooled
|
|
gptkbp:design
|
30,000 hours
Rolls-Royce_engineers
|
|
gptkbp:developer
|
$100 million
|
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gptkbp:diameter
|
1,000 mm
|
|
gptkbp:drivetrain
|
Reduction gearbox
|
|
gptkbp:emissionsStandard
|
CAEP/6
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|
gptkbp:energyEfficiency
|
High efficiency
|
|
gptkbp:engine
|
1,200 kg
Pylon mounted
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|
gptkbp:engineConfiguration
|
Twin-spool
|
|
gptkbp:enginePower
|
Single crystal alloy
|
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gptkbp:fanEvents
|
Composite material
|
|
gptkbp:firstFlight
|
1995
|
|
gptkbp:fuelCapacity
|
gptkb:Full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:fuelType
|
gptkb:Jet_A-1
Dual ignition system
|
|
gptkbp:hasContent
|
0.5 lb/hp/hr
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
AE 3007H-12
|
|
gptkbp:launched
|
Electric starter
|
|
gptkbp:length
|
1,800 mm
|
|
gptkbp:maintenance
|
4,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Rolls-Royce
|
|
gptkbp:maxSpeed
|
Mach 0.78
|
|
gptkbp:noise_level
|
Stage 4 compliant
|
|
gptkbp:numberOfStudents
|
3
|
|
gptkbp:operationalStatus
|
35,000 feet
1,500 °C
|
|
gptkbp:powerOutput
|
11,000 to 15,000 lbf
|
|
gptkbp:propulsion
|
15,000 lbf
Cascade_type
|
|
gptkbp:relatedPatent
|
gptkb:AE_3007A
gptkb:AE_3007C
AE_3007E
|
|
gptkbp:revenue
|
1995
|
|
gptkbp:rotorDiameter
|
1,000 mm
|
|
gptkbp:services
|
20,000 hours
|
|
gptkbp:totalGoals
|
Over 1,000 units
|
|
gptkbp:type
|
gptkb:Turbofan_Engine
|
|
gptkbp:usedIn
|
gptkb:Embraer_ERJ_145
|
|
gptkbp:weight
|
1,200 kg
|