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gptkbp:instance_of
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gptkb:turbofan_engine
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gptkbp:accessories
|
integrated accessories
|
|
gptkbp:application
|
regional aircraft
aircraft propulsion
|
|
gptkbp:average_temperature
|
high turbine inlet temperature
up to 2000° F
|
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gptkbp:certification
|
FAA certified
|
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gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compression_ratio
|
8:1
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gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
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gptkbp:cooling_system
|
air-cooled
|
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gptkbp:design
|
modular design
|
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gptkbp:development
|
developed from TPE331-1 U
|
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gptkbp:diameter
|
approximately 2.5 ft
|
|
gptkbp:emissions_standard
|
EPA Tier 4
|
|
gptkbp:engine
|
gptkb:TPE331_family
Brayton cycle
|
|
gptkbp:engine_configuration
|
twin-shaft
|
|
gptkbp:engine_power
|
up to 5000 hours
|
|
gptkbp:first_flight
|
1960s
|
|
gptkbp:fuel_economy
|
high efficiency
approximately 0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A
dual fuel system
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
TPE331-10 U
|
|
gptkbp:launch_platform
|
electric starter
|
|
gptkbp:legal_principle
|
gas turbine principle
|
|
gptkbp:length
|
approximately 4.5 ft
|
|
gptkbp:maintenance
|
line maintenance
500 hours
|
|
gptkbp:manufacturer
|
gptkb:Honeywell
|
|
gptkbp:market_segment
|
general aviation
|
|
gptkbp:max_speed
|
300 knots
|
|
gptkbp:noise_level
|
75 d B
|
|
gptkbp:number_of_stages
|
2
|
|
gptkbp:operational_cost
|
low operating cost
|
|
gptkbp:power_output
|
1000 shp
|
|
gptkbp:propeller
|
variable pitch
|
|
gptkbp:propulsion
|
1000 lbf
0.3 lb/hp
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:turbine_type
|
free turbine
|
|
gptkbp:type
|
turbocharged
|
|
gptkbp:weight
|
lightweight
approximately 300 lbs
|
|
gptkbp:bfsParent
|
gptkb:Honeywell_TPE331-10_GD
|
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gptkbp:bfsLayer
|
5
|