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gptkbp:instance_of
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gptkb:turbofan_engine
|
|
gptkbp:application
|
regional aircraft
|
|
gptkbp:armament
|
gptkb:6
|
|
gptkbp:certification
|
certified by Transport Canada
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compression_ratio
|
16:1
|
|
gptkbp:configuration
|
twin-shaft
|
|
gptkbp:control_system
|
gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
|
|
gptkbp:cooling_system
|
air-cooled
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:diameter
|
1,300 mm
|
|
gptkbp:elevation
|
up to 25,000 feet
|
|
gptkbp:emissions_standard
|
compliant with ICAO standards
|
|
gptkbp:engine
|
gptkb:advanced_technology
gptkb:PW100_series
commercial aviation
Brayton cycle
ongoing development
global support network
upgrade options available
|
|
gptkbp:engine_configuration
|
twin-engine
pylon-mounted
|
|
gptkbp:engine_power
|
20,000 hours
optimized for short-haul flights
proven reliability
|
|
gptkbp:engine_type
|
turboprop
multiple variants available
|
|
gptkbp:first_flight
|
gptkb:1998
|
|
gptkbp:fuel_economy
|
high
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
gptkbp:gearbox
|
reduction gearbox
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PW150 engines
|
|
gptkbp:is_tested_for
|
extensive testing
|
|
gptkbp:launched
|
electric starter
|
|
gptkbp:length
|
1,800 mm
|
|
gptkbp:maintenance
|
4,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney_Canada
|
|
gptkbp:max_speed
|
1,200 RPM
|
|
gptkbp:noise_level
|
low
|
|
gptkbp:power_output
|
1,800 k W
|
|
gptkbp:production_location
|
gptkb:Canada
|
|
gptkbp:propeller
|
2,500 mm
variable-pitch propeller
|
|
gptkbp:propulsion
|
up to 5,000 lbf
|
|
gptkbp:reliability
|
high
|
|
gptkbp:service
|
over 1,000
|
|
gptkbp:service_entry
|
gptkb:2000
|
|
gptkbp:turbine_type
|
high-pressure turbine
|
|
gptkbp:used_in
|
gptkb:Bombardier_Q400
|
|
gptkbp:water_requirement
|
1,200 lb/h
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_Canada
|
|
gptkbp:bfsLayer
|
6
|