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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:Bombardier_Q400
regional aircraft
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gptkbp:armament
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gptkb:6
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gptkbp:average_temperature
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up to 1,500 ° F
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gptkbp:certification
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gptkb:Transport_Canada
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gptkbp:combustion_system
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annular combustor
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gptkbp:compression_ratio
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16:1
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gptkbp:compression_type
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axial
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gptkbp:compressor_type
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axial
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gptkbp:configuration
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twin-shaft
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gptkbp:control_system
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gptkb:full_authority_digital_engine_control_(FADEC)
digital control system
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gptkbp:cooling_system
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air-cooled
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gptkbp:design_feature
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modular design
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gptkbp:diameter
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1,200 mm
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gptkbp:emissions_standard
|
ICAO Chapter 4
compliant with ICAO standards
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gptkbp:engine
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gptkb:PW100_family
advanced aerodynamics
cargo and passenger transport
global support network
air start
continuous improvements
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gptkbp:engine_configuration
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horizontal
inline
1 per aircraft
pylon-mounted
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gptkbp:engine_power
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high reliability
20,000 hours
optimized for short-haul flights
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gptkbp:engine_series
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gptkb:PW100_series
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gptkbp:engine_type
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turboprop
PW150 A
PW127, PW150 A
PW150 B
PW150 C
PW150 E
PW150 F
PW150 G
PW150 H
PW150 I
PW150 J
PW150 K
PW150 L
PW150 M
PW150 N
PW150 O
PW150 P
PW150 Q
PW150 R
PW150 S
PW150 T
PW150 U
PW150 V
PW150 W
PW150 X
PW150 Y
PW150 Z
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gptkbp:engine_type_code
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gptkb:PW150
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gptkbp:first_flight
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gptkb:1992
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gptkbp:fuel_capacity
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1.2 m
3.2 m
1,200 kg
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gptkbp:fuel_economy
|
high
0.5 lb/hp/hr
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gptkbp:fuel_type
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gptkb:Jet_A-1
dual channel
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gptkbp:gearbox
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reduction gearbox
planetary type
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|
https://www.w3.org/2000/01/rdf-schema#label
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PW150 engine
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gptkbp:ignition_system
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dual spark plug
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gptkbp:is_tested_for
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extensive ground testing
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gptkbp:launch_window
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air start
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gptkbp:length
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1,800 mm
3,200 mm
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gptkbp:maintenance
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3,500 hours
3,600 hours
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gptkbp:manufacturer
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gptkb:Pratt_&_Whitney_Canada
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gptkbp:market_segment
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regional aviation
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gptkbp:max_speed
|
400 knots
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gptkbp:noise_level
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low
Stage 4 compliant
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gptkbp:operating_altitude
|
25,000 feet
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gptkbp:operational_range
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up to 1,500 nautical miles
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gptkbp:power_output
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up to 5,000 shp
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gptkbp:power_source
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twin-engine aircraft
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gptkbp:propeller
|
variable pitch
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gptkbp:propeller_diameter
|
4.5 m
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gptkbp:propulsion
|
4.17
4.2:1
up to 5,000 lbf
4.2 shp/kg
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gptkbp:reduction_gearbox
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planetary type
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gptkbp:service_ceiling
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25,000 feet
30,000 feet
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gptkbp:thrust_rating
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5,000 shp
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gptkbp:training
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pilot and maintenance training available
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gptkbp:turbine_type
|
free turbine
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gptkbp:type
|
turbo-prop engine
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gptkbp:used_in
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gptkb:Bombardier_Q400
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gptkbp:weight
|
1,200 kg
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gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_Canada
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gptkbp:bfsLayer
|
6
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