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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:aircraft
|
|
gptkbp:certification
|
FAA certified
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gptkbp:compressor_type
|
axial
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gptkbp:configuration
|
free turbine
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gptkbp:control_system
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gptkb:full_authority_digital_engine_control_(FADEC)
electronic control
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gptkbp:cooling_system
|
air-cooled
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gptkbp:diameter
|
22 in
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|
gptkbp:emissions_standard
|
EPA Tier 4
|
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gptkbp:engine
|
gptkb:business_jet
modular design
Brayton cycle
developed in the 1960s
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gptkbp:engine_configuration
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pylon-mounted
twin-shaft
|
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gptkbp:engine_power
|
high reliability
5000 hours
widely used in regional aircraft
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gptkbp:engine_type
|
gptkb:turbofan_engine
gptkb:TPE331-10
|
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gptkbp:first_flight
|
gptkb:1965
|
|
gptkbp:fuel_capacity
|
dry sump
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
hydromechanical
|
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gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
TPE331-5
|
|
gptkbp:ignition_system
|
dual spark
|
|
gptkbp:is_tested_for
|
bench tested
|
|
gptkbp:launch_platform
|
starter-generator
|
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gptkbp:length
|
48 in
|
|
gptkbp:maintenance
|
300 hours
|
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gptkbp:manufacturer
|
gptkb:Honeywell
|
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gptkbp:max_continuous_power
|
950 shp
|
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gptkbp:noise_level
|
low
85 d B
|
|
gptkbp:operational_range
|
high altitude
|
|
gptkbp:power_output
|
1000 shp
|
|
gptkbp:propeller
|
variable pitch
|
|
gptkbp:propulsion
|
optional
3.33
0.3 lb/shp
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:turbine_type
|
single stage
|
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gptkbp:warranty
|
2 years
|
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gptkbp:water_requirement
|
replaceable
|
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gptkbp:weight
|
300 lb
|
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gptkbp:bfsParent
|
gptkb:Honeywell_TPE331
gptkb:TPE331_family
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gptkbp:bfsLayer
|
6
|