|
gptkbp:instance_of
|
gptkb:turbofan_engine
|
|
gptkbp:bypass_ratio
|
9:1
|
|
gptkbp:cancellation_reason
|
geared architecture
|
|
gptkbp:compressor_type
|
fan, high-pressure compressor
|
|
gptkbp:configuration
|
twin-spool
|
|
gptkbp:control_system
|
gptkb:FADEC
|
|
gptkbp:cooling_system
|
advanced cooling techniques
|
|
gptkbp:customer_support
|
gptkb:Bombardier
|
|
gptkbp:design_purpose
|
fuel efficiency
|
|
gptkbp:development_cost
|
$1 billion
|
|
gptkbp:diameter
|
1,600 mm
1,500 mm
|
|
gptkbp:emissions_standard
|
low emissions
ICAO Chapter 4
|
|
gptkbp:engine
|
gptkb:PW1000_G
regional aircraft
|
|
gptkbp:engine_configuration
|
high bypass ratio
18,000 lbf
|
|
gptkbp:engine_power
|
high reliability
high efficiency
|
|
gptkbp:engine_type
|
turbofan
|
|
gptkbp:first_flight
|
gptkb:2013
|
|
gptkbp:fuel_capacity
|
1,600 mm
1,200 kg
3,200 mm
|
|
gptkbp:fuel_economy
|
0.5 lb/hp/hr
|
|
gptkbp:fuel_type
|
gptkb:Jet_A-1
|
|
gptkbp:has_programs
|
Pure Power
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
PW1200 G-10
|
|
gptkbp:length
|
3,200 mm
|
|
gptkbp:maintenance
|
5,000 hours
|
|
gptkbp:manufacturer
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:market_segment
|
regional jets
|
|
gptkbp:noise_level
|
low noise
|
|
gptkbp:operational_use
|
commercial aviation
|
|
gptkbp:propulsion
|
18,000 lbf
|
|
gptkbp:related_aircraft
|
CSeries family
|
|
gptkbp:service_ceiling
|
41,000 ft
|
|
gptkbp:turbine_type
|
high-pressure turbine, low-pressure turbine
|
|
gptkbp:type
|
geared turbofan
|
|
gptkbp:used_in
|
gptkb:Bombardier_CSeries
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:Pratt_&_Whitney_PW1200_G
|
|
gptkbp:bfsLayer
|
6
|