Properties (55)
Predicate | Object |
---|---|
gptkbp:instanceOf |
turbofan engine
|
gptkbp:aircraft |
transport aircraft
|
gptkbp:application |
military transport aircraft
civil transport aircraft |
gptkbp:compressionRatio |
single-stage fan and 6-stage axial compressor
|
gptkbp:controls |
gptkb:full_authority_digital_engine_control_(FADEC)
|
gptkbp:coolingSystem |
air-cooled turbine blades
|
gptkbp:design |
25,000 hours
|
gptkbp:design_feature |
modular design
advanced materials high reliability low maintenance costs high bypass ratio low specific fuel consumption |
gptkbp:developer |
based_on_the_D-30KP_engine
|
gptkbp:diameter |
2.9 m
1.1 m |
gptkbp:emissionsStandard |
annular combustor
compliant_with_ICAO_standards |
gptkbp:engineConfiguration |
twin-engine configuration
|
gptkbp:engineType |
two-stage high-pressure turbine
two-stage low-pressure turbine |
gptkbp:first_appearance |
2016
|
gptkbp:firstFlight |
2013
|
gptkbp:fuel_capacity |
high fuel efficiency
|
gptkbp:fuelType |
gptkb:Jet_A-1
|
https://www.w3.org/2000/01/rdf-schema#label |
WS-20 turbofan engine
|
gptkbp:is_used_in |
gptkb:Xian_Y-20
|
gptkbp:length |
3.8 m
|
gptkbp:maintenance |
5,000 hours
|
gptkbp:manufacturer |
gptkb:Aero_Engine_Corporation_of_China
|
gptkbp:market |
growing_demand_in_Asia
|
gptkbp:maximum_speed |
0.8 Mach
|
gptkbp:noise_level |
low noise emissions
|
gptkbp:operational_status |
in service since 2016
|
gptkbp:operationalRange |
long-range missions
|
gptkbp:performance |
reduced environmental impact
increased payload capacity improved climb rate enhanced operational flexibility adaptable to different aircraft designs better takeoff performance competitive with Western engines improved thrust performance optimized for high altitude operations suitable for various mission profiles |
gptkbp:produces |
2000
|
gptkbp:propulsion |
4.64
13,000 kgf |
gptkbp:related_engine |
gptkb:D-30KP
WS-10 WS-15 |
gptkbp:service_ceiling |
12,000 m
|
gptkbp:type |
high-bypass turbofan
|
gptkbp:weight |
2,800 kg
|