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gptkbp:instance_of
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gptkb:turbofan_engine
|
|
gptkbp:application
|
regional aircraft
|
|
gptkbp:armament
|
gptkb:4
|
|
gptkbp:compression_ratio
|
8:1
|
|
gptkbp:configuration
|
free turbine
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
electronic control system
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:diameter
|
approximately 2.5 ft
|
|
gptkbp:elevation
|
up to 25,000 ft
|
|
gptkbp:emissions_standard
|
meets FAA regulations
|
|
gptkbp:engine
|
advanced materials
lightweight design
high reliability
low maintenance
Brayton cycle
high efficiency
reliable operation
low operating costs
versatile applications
robust performance
|
|
gptkbp:engine_configuration
|
modular design
1,000 shp
horizontal layout
twin-shaft
|
|
gptkbp:engine_displacement
|
approximately 1,200 cu in
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
|
|
gptkbp:first_introduced
|
1960s
|
|
gptkbp:fuel_economy
|
approximately 600 lb/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
dual fuel pumps
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
TPE331-10
|
|
gptkbp:ignition_system
|
dual ignition
|
|
gptkbp:launch_platform
|
electric starter
|
|
gptkbp:length
|
approximately 4.5 ft
|
|
gptkbp:maintenance
|
300 hours
|
|
gptkbp:manufacturer
|
gptkb:Honeywell
|
|
gptkbp:max_speed
|
250 knots
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:notable_users
|
gptkb:Cessna
gptkb:Beechcraft
gptkb:Piper_Aircraft
gptkb:Fairchild
gptkb:Dornier
|
|
gptkbp:power_output
|
1000 shp
|
|
gptkbp:propeller
|
constant speed propeller
|
|
gptkbp:propulsion
|
3.33:1
3.33 hp/lb
|
|
gptkbp:service
|
up to 10,000 hours
|
|
gptkbp:type
|
turbocharged engine
|
|
gptkbp:used_in
|
gptkb:aircraft
|
|
gptkbp:variant
|
TPE331-5, TPE331-12
|
|
gptkbp:weight
|
approximately 300 lbs
|
|
gptkbp:bfsParent
|
gptkb:Honeywell_TPE331-10_GD
|
|
gptkbp:bfsLayer
|
5
|