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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:military_aircraft
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|
gptkbp:collaboration
|
with various Chinese aerospace companies
|
|
gptkbp:combustor_type
|
annular combustor
|
|
gptkbp:compressor_type
|
3 axial and 1 centrifugal
|
|
gptkbp:control_system
|
digital control system
|
|
gptkbp:cooling_system
|
air-cooled
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|
gptkbp:design_philosophy
|
indigenous development
|
|
gptkbp:designed_by
|
gptkb:Shenyang_Liming_Aircraft_Engine_Company
|
|
gptkbp:development
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gptkb:1980s
|
|
gptkbp:development_cost
|
significant investment
|
|
gptkbp:diameter
|
1,000 mm
|
|
gptkbp:emissions_standard
|
meets modern standards
|
|
gptkbp:engine
|
WS series engines
|
|
gptkbp:engine_configuration
|
twin-spool
|
|
gptkbp:export_markets
|
limited due to military applications
|
|
gptkbp:facilities
|
utilized in various test centers
|
|
gptkbp:fuel_type
|
Aviation kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
WS-10 A Taihang
|
|
gptkbp:influence
|
gptkb:Chinese_aerospace_industry
|
|
gptkbp:inspired_by
|
Russian AL-31 F engine
|
|
gptkbp:integration
|
integrated into multiple aircraft types
|
|
gptkbp:length
|
3,800 mm
|
|
gptkbp:maintenance
|
requires specialized training
|
|
gptkbp:market
|
domestic and export
|
|
gptkbp:notable_feature
|
gptkb:full_authority_digital_engine_control_(FADEC)
|
|
gptkbp:operational_since
|
gptkb:2000
|
|
gptkbp:operational_use
|
gptkb:People's_Liberation_Army_Air_Force
|
|
gptkbp:original_run
|
gptkb:1996
|
|
gptkbp:part_of
|
China's military modernization efforts
|
|
gptkbp:performance
|
evaluated in various conditions
high thrust and efficiency
|
|
gptkbp:project
|
prototype testing
WS-15 and WS-20 engines
|
|
gptkbp:propulsion
|
8.67
not equipped
130 k N
|
|
gptkbp:related_aircraft
|
Chinese fighter aircraft
|
|
gptkbp:related_to
|
WS-15 engine
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:replaced_by
|
Russian engines in Chinese aircraft
|
|
gptkbp:research_and_development
|
ongoing improvements
|
|
gptkbp:strategic_importance
|
for national defense
|
|
gptkbp:successor
|
WS-6 engine
|
|
gptkbp:turbine_type
|
2 high-pressure and 1 low-pressure
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:used_in
|
gptkb:Chengdu_J-10
gptkb:Shenyang_J-11
gptkb:Shenyang_FC-31
|
|
gptkbp:weight
|
about 1,500 kg
|
|
gptkbp:bfsParent
|
gptkb:Chengdu_J-10
|
|
gptkbp:bfsLayer
|
6
|