WS-20 turbofan engine

GPTKB entity

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