|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:application
|
business aviation
|
|
gptkbp:armament
|
gptkb:4
|
|
gptkbp:average_temperature
|
-40 to 50 ° C
|
|
gptkbp:certification
|
FAA certified
|
|
gptkbp:compression_ratio
|
8.5:1
|
|
gptkbp:compressor_type
|
axial compressor
|
|
gptkbp:configuration
|
free turbine
|
|
gptkbp:control_system
|
digital engine control
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design
|
5000 hours
|
|
gptkbp:diameter
|
0.5 m
|
|
gptkbp:emissions_standard
|
low
|
|
gptkbp:engine
|
gptkb:PT6_family
Brayton cycle
|
|
gptkbp:engine_configuration
|
twin-spool
pylon mounted
|
|
gptkbp:engine_type
|
turboprop
|
|
gptkbp:first_flight
|
gptkb:1963
|
|
gptkbp:fuel_economy
|
high
|
|
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
|
PT6 A-70
|
|
gptkbp:launch_window
|
electric starter
|
|
gptkbp:length
|
1.5 m
|
|
gptkbp:maintenance
|
2000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
|
|
gptkbp:market_segment
|
regional aviation
|
|
gptkbp:max_speed
|
gptkb:2000
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:operational_range
|
2000 km
|
|
gptkbp:power_output
|
700 shp
|
|
gptkbp:propeller
|
constant speed propeller
|
|
gptkbp:propulsion
|
4.67
0.21 kg/shp
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service_ceiling
|
25,000 ft
|
|
gptkbp:turbine_type
|
single stage turbine
|
|
gptkbp:type
|
turbo-prop engine
|
|
gptkbp:used_in
|
gptkb:aircraft
|
|
gptkbp:water_requirement
|
50-60 lb/hr
|
|
gptkbp:weight
|
150 kg
|
|
gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_Canada_PT6_A-42
|
|
gptkbp:bfsLayer
|
7
|