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gptkbp:instance_of
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gptkb:turbofan_engine
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gptkbp:application
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gptkb:business_jet
|
|
gptkbp:certification
|
FAA certified
NOx compliant
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gptkbp:combustor_type
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annular
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gptkbp:compressor_type
|
axial-flow
|
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gptkbp:control_system
|
digital control system
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gptkbp:cooling_system
|
air-cooled
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gptkbp:design_features
|
high bypass ratio
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gptkbp:diameter
|
2.5 ft
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gptkbp:engine
|
gptkb:TFE731_family
advanced aerodynamics
modern technology
Brayton cycle
various aircraft models
available upgrades
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gptkbp:engine_configuration
|
twin-spool
detailed specifications available.
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|
gptkbp:engine_power
|
high reliability
reliable performance
up to 8,000 hours
|
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gptkbp:engine_type
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gptkb:turbofan_engine
TFE731-40, TFE731-50
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gptkbp:first_flight
|
gptkb:1980
|
|
gptkbp:fuel_economy
|
high efficiency
0.5 lb/hp/hr
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gptkbp:fuel_type
|
gptkb:Jet_A
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Honeywell TFE731-60 BR
|
|
gptkbp:launched
|
electric starter
|
|
gptkbp:legal_principle
|
gptkb:Cooler
|
|
gptkbp:length
|
4.5 ft
|
|
gptkbp:maintenance
|
4,000 hours
scheduled maintenance required
|
|
gptkbp:manufacturer
|
gptkb:Honeywell
|
|
gptkbp:maximum_operating_temperature
|
1,000 ° F
|
|
gptkbp:noise_level
|
Stage 3
|
|
gptkbp:notable_applications
|
gptkb:Cessna_Citation_series
|
|
gptkbp:number_of_stages
|
gptkb:10
|
|
gptkbp:power_output
|
3,500 lbf
|
|
gptkbp:propulsion
|
3,500 lbf
|
|
gptkbp:service_ceiling
|
41,000 ft
|
|
gptkbp:turbine_type
|
two-stage
|
|
gptkbp:weight
|
1,200 lb
|
|
gptkbp:bfsParent
|
gptkb:Falcon_2000_S
|
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gptkbp:bfsLayer
|
7
|